nasa

us national archives

exercise

kennedy space center

cape canaveral

tandem

rocket

tandem thrust

thrust

1,071 media by topic ∙ page 1 of 11
X-15 #2 just after launch. Public domain image of NASA aircraft.

X-15 #2 just after launch. Public domain image of NASA aircraft.

Description: The X-15 #2 (56-6671) launches away from the B-52 mothership with its rocket engine ignited. The white patches near the middle of the ship are frost from the liquid oxygen used in the propulsion sy... More

Amulet of fist with thumb thrust between first two fingers

Amulet of fist with thumb thrust between first two fingers

Public domain photograph of 3d object, free to use, no copyright restrictions image - Picryl description.

CERAMIC MATRIX COMPOSITE THRUST CELLS GRC-2001-C-00536

CERAMIC MATRIX COMPOSITE THRUST CELLS GRC-2001-C-00536

CERAMIC MATRIX COMPOSITE THRUST CELLS Public domain photograph related to NASA research activity, space exploration, free to use, no copyright restrictions image - Picryl description

John is thrust into prison from BL Add 42497, f. 1ev

John is thrust into prison from BL Add 42497, f. 1ev

Scene with caption above of John the Baptist being thrust into prison by two men. Image taken from f. 1ev of Scenes from the Life of John the Baptist (possibly illustrating the Hortus Deliciarum?), a Flabellum ... More

Two angels proclaiming the day of judgement; the Son of Man (Christ) with a sickle (scythe) and a cross; an angel comes out of the temple crying to him to thrust the sickle into the earth and to reap; a second angel, who controls the fire, cries from his altar to the third angel, who carries a sickle, to thrust his sickle into the earth and gather the vine (2nd of 2)

Two angels proclaiming the day of judgement; the Son of Man (Christ) w...

Public domain scan of a medieval manuscript, free to use, no copyright restrictions image - Picryl description.

Two angels proclaiming the day of judgement; the Son of Man (Christ) with a sickle (scythe) and a cross; an angel comes out of the temple crying to him to thrust the sickle into the earth and to reap; a second angel, who controls the fire, cries from his altar to the third angel, who carries a sickle, to thrust his sickle into the earth and gather the vine (2nd of 2)

Two angels proclaiming the day of judgement; the Son of Man (Christ) w...

Public domain scan of a medieval manuscript, free to use, no copyright restrictions image - Picryl description.

The Knife Thrust, Adriaen van Ostade

The Knife Thrust, Adriaen van Ostade

Adriaen van Ostade (Dutch, Haarlem 1610–1685 Haarlem) Public domain photograph of 17th century Dutch drawing, free to use, no copyright restrictions image - Picryl description

The Knife Thrust, Adriaen van Ostade

The Knife Thrust, Adriaen van Ostade

Adriaen van Ostade (Dutch, Haarlem 1610–1685 Haarlem) Public domain photograph of 17th-18th century drawing, free to use, no copyright restrictions image - Picryl description

Raker on a Wisconsin cranberry marsh. With a swinging motion the prongs of the rake are thrust under the lowest layer of berries, and with the left hand, the rake is pulled forward and up, completing the arc. Each raker empties his berries into a box behind him. When full these are carried off by porters. Location: Grand Rapids, Wisconsin. / Photo by courtesy of Mr. Andrew Searles the owner.

Raker on a Wisconsin cranberry marsh. With a swinging motion the prong...

Public domain photograph - historical image of Wisconsin, United States, free to use, no copyright restrictions image - Picryl description

Raker on a Wisconsin cranberry marsh. With a swinging motion the prongs of the rake are thrust under the lowest layer of berries, and with the left hand, the rake is pulled forward and up, completing the arc. Each raker empties his berries into a box behind him. When full these are carried off by porters. Location: Grand Rapids, Wisconsin. / Photo by courtesy of Mr. Andrew Searles the owner.

Raker on a Wisconsin cranberry marsh. With a swinging motion the prong...

Picryl description: Public domain image of working farmers, agriculture, farm, 20th century, free to use, no copyright restrictions.

The 42nd Capricornia Battalion, Sergeant Major wipes the sweat from one of his soldier's brow during the annual commemoration of the Australian/New Zealand Army Corps (ANZAC) Day held in Rockhampton, Australia, on April 25, 2001. The annual parade honors the 35,000 soldiers who were killed or wounded during the Gallipoli landing on April 25, 1915. ANZAC Day also honors the brave men and women of Australia and New Zealand who have defended freedom in conflicts around the world. The commemoration occurred during TANDEM THRUST 2001, which is a combined US-Australian crisis action planning and contingency response military training exercise involving more than 27,000 Soldiers, Sailors,...

The 42nd Capricornia Battalion, Sergeant Major wipes the sweat from on...

The original finding aid described this photograph as: [Complete] Scene Caption: The 42nd Capricornia Battalion, Sergeant Major wipes the sweat from one of his soldier's brow during the annual commemoration of... More

Members of the Naval Construction Battalion One (NCB1) Seabees from Gulf Port, Mississippi, forward deployed to Guam participate in the Australian/New Zealand Army Corps (ANZAC) Day parade an annual cerebration held in Rockhampton, Australia, on April 5, 001. The annual parade honors the 35,000 soldiers who were killed or wounded during the Gallipoli landing on April 5, 1915. ANZAC Day also honors the brave men and women of Australia and New Zealand who have defended freedom in conflicts around the world. The commemoration occurred during TANDEM THRUST 001, which is a combined US-Australian crisis action planning and contingency response military training exercise involving more than...

Members of the Naval Construction Battalion One (NCB1) Seabees from Gu...

The original finding aid described this photograph as: [Complete] Scene Caption: Members of the Naval Construction Battalion One (NCB1) Seabees from Gulf Port, Mississippi, forward deployed to Guam participate... More

Members of the US Marine Corps Honor Guard and Navy Seabees participate in the Australian/New Zealand Army Corps (ANZAC) parade during the ANZAC Day commemoration held in Rockhampton, Australia on April 25, 2001. The annual parade honors the 35,000 soldiers who were killed or wounded during the Gallipoli landing on April 25, 1915. ANZAC Day also honors the brave men and women of Australia and New Zealand who have defended freedom in conflicts around the world. The commemoration occurred during TANDEM THRUST 2001, which is a combined US-Australian crisis action planning and contingency response military training exercise involving more than 27,000 Soldiers, Sailors, Airmen and Marines

Members of the US Marine Corps Honor Guard and Navy Seabees participat...

The original finding aid described this photograph as: Subject Operation/Series: TANDEM THRUST 2001 Base: Rockhampton State: Queensland Country: Australia (AUS) Scene Camera Operator: SSGT Jeremy Lock, USA... More

Participants in the Australian/New Zealand Army Corps (ANZAC) parade march during the commemoration held in Rockhampton, Australia, on April 25, 2001. The annual parade honors the 35,000 soldiers who were killed or wounded during the Gallipoli landing on April 25, 1915. ANZAC Day also honors the brave men and women of Australia and New Zealand who have defended freedom in conflicts around the world. The commemoration occurred during TANDEM THRUST 2001, which is a combined US-Australian crisis action planning and contingency response military training exercise involving more than 27,000 Soldiers, Sailors, Airmen and Marines

Participants in the Australian/New Zealand Army Corps (ANZAC) parade m...

The original finding aid described this photograph as: Subject Operation/Series: TANDEM THRUST 2001 Base: Rockhampton State: Queensland Country: Australia (AUS) Scene Camera Operator: SSGT Jeremy Lock, USA... More

"We closed the road to Paris - we're on our way to Berlin" Every bond you buy of the 4th Liberty Loan is a bayonet thrust at the Kaiser / / Steffan.

"We closed the road to Paris - we're on our way to Berlin" Every bond ...

Poster showing Kaiser Wilhelm attempting to walk across a sea of soldiers with bayonets aloft. Plates by Baltimore, Maryland Engraving Co.

Airplanes - Manufacturing Plants - Fitting gear covering. Thrust end clamp

Airplanes - Manufacturing Plants - Fitting gear covering. Thrust end c...

Date Taken: 4/16/1917 Photographer: Curtiss Aeroplane Co. Airplanes - Manufacturing Plants

Airplanes - Engines - Curtiss aeroplane and motor corporation, Buffalo, N.Y. Progressive assembly operation No. 3 fitting gear cover and thrust end clamp. Curtiss Aeroplane & Motor Corp

Airplanes - Engines - Curtiss aeroplane and motor corporation, Buffalo...

Photographer: Curtis Aeroplane & Motor Corp. Airplanes - Engines Public domain photograph of aircraft engine, free to use, no copyright restrictions image - Picryl description

Airplanes - Engines - Manufacturing Curtiss Ox-5 airplane engines at the Willy-s Morrow Plant, Elmira, New York. Tapping gear and thrust ends

Airplanes - Engines - Manufacturing Curtiss Ox-5 airplane engines at t...

Photographer: Willys-Morrow Plant Airplanes - Engines Public domain photograph of aircraft engine, free to use, no copyright restrictions image - Picryl description

Airplanes - Instruments - Method of testing aeroplane engine bearers for thrust loading. Forest Products Laboratory, Madison, Wis

Airplanes - Instruments - Method of testing aeroplane engine bearers f...

Photographer: Forest Products Laboratory, Madison, Wis. Airplanes - Instruments Public domain photograph related to the United States in World War One, free to use, no copyright restrictions image - Picryl description

Airplanes - Manufacturing Plants - Manufacturing Curtiss OX-5 Airplane Engines at the Willys-Morrow Co. Plant, Elmira, New York. Drilling holes in thrust end

Airplanes - Manufacturing Plants - Manufacturing Curtiss OX-5 Airplane...

Photographer: From the Willys-Morrow Co. Airplanes - Manufacturing Plants Public domain photograph related to the United States in World War One, free to use, no copyright restrictions image - Picryl description

Airplanes - Engines - Manufacturing Curtiss Ox-5 airplane engines at the Willy-s Morrow Plant, Elmira, New York. Crank shaft thrust bearing cover

Airplanes - Engines - Manufacturing Curtiss Ox-5 airplane engines at t...

Photographer: Willys-Morrow Plant Airplanes - Engines Public domain photograph related to the United States in World War One, free to use, no copyright restrictions image - Picryl description

Airplanes - Engines - Manufacturing Curtiss Ox-5 airplane engines at the Willy-s Morrow Plant, Elmira, New York. Thrust bearing lock nut

Airplanes - Engines - Manufacturing Curtiss Ox-5 airplane engines at t...

Photographer: Willys-Morrow Plant Airplanes - Engines Public domain photograph related to the United States in World War One, free to use, no copyright restrictions image - Picryl description

Great Falls, Montana. Electolytic copper refinery of Anaconda Copper Mining Company. Inspecting the electrolytic process; by means of this tool which is thrust down and towards the inspector he is able to determine if deposition of copper is proceeding at the normal rage and if there are any short circuits

Great Falls, Montana. Electolytic copper refinery of Anaconda Copper M...

Picryl description: Public domain image of an industrial building, factory, workshop, workers, 19th-20th century, free to use, no copyright restrictions.

Great Falls, Montana. Electrolytic refinery of Anaconda Copper Mining Company. Inspecting the electrolytic process. By means of this tool which is thrust down and towards the inspector he is able to determine if deposition of copper is proceeding at the normal rate and if there are any short circuits present

Great Falls, Montana. Electrolytic refinery of Anaconda Copper Mining ...

Picryl description: Public domain image of a mine, mining, free to use, no copyright restrictions.

Great Falls, Montana. Electrolytic refinery of Anaconda Copper Mining Company. Inspecting the electrolytic process. By means of this tool which is thrust down and towards the inspector he is able to determine if deposition of copper is proceeding at the normal rate and if there are any short circuits present

Great Falls, Montana. Electrolytic refinery of Anaconda Copper Mining ...

Public domain photograph of United States agriculture in the 1930s, country, farmer, farm, great depression, migration, dust bowl refugees, free to use, no copyright restrictions image - Picryl description

Great Falls, Montana. Electrolytic refinery of Anaconda Copper Mining Company. Inspecting the electrolytic process. By means of this tool which is thrust down and towards the inspector he is able to determine if deposition of copper is proceeding at the normal rate and if there are any short circuits present

Great Falls, Montana. Electrolytic refinery of Anaconda Copper Mining ...

Picryl description: Public domain image of a worker, labor, factory, plant, manufacture, industrial facility, 1930s, mid-20th-century industrial photo, free to use, no copyright restrictions.

Great Falls, Montana. Electrolytic copper refinery of Anaconda Copper Mining Company. Inspecting the electolytic process. By means of this tool which is thrust down and towards the inspector he is able to detemine if deposition of copper is proceeding at the normal rate and if there are any short circuits present

Great Falls, Montana. Electrolytic copper refinery of Anaconda Copper ...

Picryl description: Public domain image of an industrial building, factory, workshop, workers, 20th century, free to use, no copyright restrictions.

Pittsburgh, Pennsylvania. Lower bracket of the 30,000 kilowatt waterwheel generator which Westinghouse Electric Company is manufacturing for the Watts Bar Dam of the Tennessee Valley Authority (TVA), from underneath, showing hole through which the shaft is passed. The bracket supports the thrust bearing on which rests the entire rotating mechanism of the generator. It has eight arms which bear the brunt of the generator's weight. The bracket weighs 107,500 pounds

Pittsburgh, Pennsylvania. Lower bracket of the 30,000 kilowatt waterwh...

Public domain photograph of Pennsylvania in 1930s, free to use, no copyright restrictions image - Picryl description

Two US Marine Corps (USMC) CH-46 Sea Knight helicopters, Marine Medium Helicopter Squadron 262 (HMM-262), Futenma, Japan, deploy with evacuees during a simulated non-combatant evacuation operation (NEO) at US Naval Forces Marianas Support Activity, Guam. The simulated NEO is part of Exercise TANDEM THRUST 2003, a joint military endeavor including forces from the United States, Canada and Australia

Two US Marine Corps (USMC) CH-46 Sea Knight helicopters, Marine Medium...

The original finding aid described this photograph as: Base: US Naval Forces, Marianas State: Guam (GU) Country: Northern Mariana Islands (MNP) Scene Camera Operator: TSGT Steve Cline, USAF Release Status:... More

NACA AMES ENGINEERS: Seth B. ANDERSON AND NACA AMES PILOT Gorge E. COOPER WITH W.E. RHOADES, ROBERT McIVER, MICHAEL CASSENLY OF UNITED AIRLINES. Visit Ames to dicuss Thrust Reverser Problems. ARC-1957-A-23176

NACA AMES ENGINEERS: Seth B. ANDERSON AND NACA AMES PILOT Gorge E. CO...

NACA AMES ENGINEERS: Seth B. ANDERSON AND NACA AMES PILOT Gorge E. COOPER WITH W.E. RHOADES, ROBERT McIVER, MICHAEL CASSENLY OF UNITED AIRLINES. Visit Ames to dicuss Thrust Reverser Problems.

NACA Photographer Thrust reverser on F-94C-1 (AF50-956 NACA 156) Starfire (l to R) Air Force Major E. Sommerich; Ames Engineer Seth Anderson, Lt. Col. Tavasti; and Ames Chief test pilot George Cooper discussing phases of flight evaluation tests. Note: Used in publication in Flight Research at Ames; 57 Years of Development and Validation of Aeronautical Technology NASA SP-1998-3300 fig 91 ARC-1958-A-23928

NACA Photographer Thrust reverser on F-94C-1 (AF50-956 NACA 156) Starf...

NACA Photographer Thrust reverser on F-94C-1 (AF50-956 NACA 156) Starfire (l to R) Air Force Major E. Sommerich; Ames Engineer Seth Anderson, Lt. Col. Tavasti; and Ames Chief test pilot George Cooper discussin... More

CAPE CANAVERAL, Fla. - With more than 12 times the thrust produced by a Boeing 747 jet aircraft, the Constellation Program's Ares I-X test rocket roars off Launch Complex 39B at NASA's Kennedy Space Center in Florida. The rocket produces 2.96 million pounds of thrust at liftoff and goes supersonic in 39 seconds. Liftoff of the 6-minute flight test was at 11:30 a.m. EDT Oct. 28. This was the first launch from Kennedy's pads of a vehicle other than the space shuttle since the Apollo Program's Saturn rockets were retired. The parts used to make the Ares I-X booster flew on 30 different shuttle missions ranging from STS-29 in 1989 to STS-106 in 2000. The data returned from more than 700 sensors throughout the rocket will be used to refine the design of future launch vehicles and bring NASA one step closer to reaching its exploration goals. For information on the Ares I-X vehicle and flight test, visit http://www.nasa.gov/aresIX. Photo credit: NASA/Jim Grossmann KSC-2009-5933

CAPE CANAVERAL, Fla. - With more than 12 times the thrust produced by ...

CAPE CANAVERAL, Fla. - With more than 12 times the thrust produced by a Boeing 747 jet aircraft, the Constellation Program's Ares I-X test rocket roars off Launch Complex 39B at NASA's Kennedy Space Center in F... More

CAPE CANAVERAL, Fla. – The first stage ignited on NASA’s Ares I-X test rocket at Launch Pad 39B at NASA's Kennedy Space Center in Florida at 11:30 a.m. EDT on Oct. 28. The rocket produces 2.96 million pounds of thrust at liftoff and reaches a speed of 100 mph in eight seconds. This was the first launch from Kennedy's pads of a vehicle other than the space shuttle since the Apollo Program's Saturn rockets were retired. The parts used to make the Ares I-X booster flew on 30 different shuttle missions ranging from STS-29 in 1989 to STS-106 in 2000. The data returned from more than 700 sensors throughout the rocket will be used to refine the design of future launch vehicles and bring NASA one step closer to reaching its exploration goals. For information on the Ares I-X vehicle and flight test, visit http://www.nasa.gov/aresIX. Photo credit: NASA/Sandra Joseph and Kevin O'Connell KSC-2009-5987

CAPE CANAVERAL, Fla. – The first stage ignited on NASA’s Ares I-X test...

CAPE CANAVERAL, Fla. – The first stage ignited on NASA’s Ares I-X test rocket at Launch Pad 39B at NASA's Kennedy Space Center in Florida at 11:30 a.m. EDT on Oct. 28. The rocket produces 2.96 million pounds of... More

CAPE CANAVERAL, Fla. -- Repair work to space shuttle Discovery's external fuel tank begins in the Vehicle Assembly Building at NASA's Kennedy Space Center in Florida. Technicians will modify 32 support beams, called stringers, on the tank's intertank region by fitting pieces of metal, called radius blocks, over the stringers' edges where they attach to the thrust panel area. The thrust panel is where the tank meets the two solid rocket boosters and sees the most stress during the flight into orbit. After the modifications and additional scans of the stringers are complete, foam insulation will be re-applied. Discovery's next launch opportunity to the International Space Station on the STS-133 mission is no earlier than Feb. 3, 2011. For more information on STS-133, visit www.nasa.gov/mission_pages/shuttle/shuttlemissions/sts133/. Photo credit: NASA/Jack Pfaller KSC-2011-1000

CAPE CANAVERAL, Fla. -- Repair work to space shuttle Discovery's exter...

CAPE CANAVERAL, Fla. -- Repair work to space shuttle Discovery's external fuel tank begins in the Vehicle Assembly Building at NASA's Kennedy Space Center in Florida. Technicians will modify 32 support beams, c... More

Saturn I H-1 engine - Saturn Apollo Program

Saturn I H-1 engine - Saturn Apollo Program

H-1 engine characteristics: The H-1 engine was developed under the management of the Marshall Space Flight Center (MSFC). The cluster of eight H-1 engines was used to power the first stage of the Saturn I (S-I ... More

Saturn Apollo Program - F-1 rocket engine

Saturn Apollo Program - F-1 rocket engine

This chart provides the vital statistics for the F-1 rocket engine. Developed by Rocketdyne, under the direction of the Marshall Space Flight Center, the F-1 engine was utilized in a cluster of five engines to ... More

Saturn V J-2 engine - Saturn Apollo Program

Saturn V J-2 engine - Saturn Apollo Program

This chart is an illustration of J-2 Engine characteristics. A cluster of five J-2 engines powered the Saturn V S-II (second) stage with each engine providing a thrust of 200,000 pounds. A single J-2 engine pow... More

Saturn I - Saturn Apollo Program - eight H-1 engines

Saturn I - Saturn Apollo Program - eight H-1 engines

A Cluster of eight H-1 engines were used to thrust the first stage of Saturn I (S-I stage) and Saturn IB (S-IB stage). The engines were arranged in a double pattern. Four engines, located inboard, were fixed in... More

CAPE CANAVERAL, Fla. – Inside Orbiter Processing Facility-1 at NASA’s Kennedy Space Center in Florida, the left orbital maneuvering system, or OMS, pod has been installed onto space shuttle Atlantis. The OMS provided the shuttle with thrust for orbit insertion, rendezvous and deorbit, and could provide up to 1,000 pounds of propellant to the aft reaction control system. The OMS is housed in two independent pods located on each side of the shuttle’s aft fuselage. Each pod contains one OMS engine and the hardware needed to pressurize, store and distribute the propellants to perform the velocity maneuvers. Atlantis’ OMS pods were removed and sent to White Sands Test Facility in New Mexico to be cleaned of residual toxic propellant. The work is part of the Space Shuttle Program’s transition and retirement processing of the space shuttle fleet. A groundbreaking was held Jan. 18 for Atlantis’ future home, a 65,000-square-foot exhibit hall in Shuttle Plaza at the Kennedy Space Center Visitor Complex. Atlantis is scheduled to roll over to the visitor complex in November in preparation for the exhibit’s grand opening in July 2013. For more information, visit http://www.nasa.gov/transition. Photo credit: NASA/Ben Smegelsky KSC-2012-3348

CAPE CANAVERAL, Fla. – Inside Orbiter Processing Facility-1 at NASA’s ...

CAPE CANAVERAL, Fla. – Inside Orbiter Processing Facility-1 at NASA’s Kennedy Space Center in Florida, the left orbital maneuvering system, or OMS, pod has been installed onto space shuttle Atlantis. The OMS pr... More

CAPE CANAVERAL, Fla. -- In the Space Shuttle Main Engine Processing Facility at NASA's Kennedy Space Center in Florida, two of six space shuttle main engines are prepared for the STS-134 and STS-335 missions. Postflight inspections and maintenance of each engine are conducted in the facility between shuttle missions by Pratt & Whitney Rocketdyne aerospace technicians. Three main engines are clustered at the aft end of the shuttle and have a combined thrust of more than 1.2 million pounds. Each engine utilizes liquid hydrogen for fuel and liquid oxygen as oxidizer and operates during the entire eight-and-a-half minute ride to orbit. Space shuttle Endeavour's STS-134 mission is the final planned mission of the Space Shuttle Program and will deliver the Alpha Magnetic Spectrometer, as well as critical spare components, to the International Space Station next year. Shuttle Atlantis will be prepared for STS-335, which is the planned "launch on need," or potential rescue mission, for Endeavour's STS-134 mission. For information, visit www.nasa.gov/shuttle. Photo credit: NASA/Jack Pfaller KSC-2010-4670

CAPE CANAVERAL, Fla. -- In the Space Shuttle Main Engine Processing Fa...

CAPE CANAVERAL, Fla. -- In the Space Shuttle Main Engine Processing Facility at NASA's Kennedy Space Center in Florida, two of six space shuttle main engines are prepared for the STS-134 and STS-335 missions. P... More

CAPE CANAVERAL, Fla. – NASA's Ares I-X test rocket ignites its first stage at Launch Pad 39B at NASA's Kennedy Space Center in Florida at 11:30 a.m. EDT on Oct. 28. The Constellation Program's 327-foot-tall rocket produces 2.96 million pounds of thrust at liftoff and reaches a speed of 100 mph in eight seconds. This was the first launch from Kennedy's pads of a vehicle other than the space shuttle since the Apollo Program's Saturn rockets were retired. The parts used to make the Ares I-X booster flew on 30 different shuttle missions ranging from STS-29 in 1989 to STS-106 in 2000. The data returned from more than 700 sensors throughout the rocket will be used to refine the design of future launch vehicles and bring NASA one step closer to reaching its exploration goals. For information on the Ares I-X vehicle and flight test, visit http://www.nasa.gov/aresIX. Photo credit: NASA/ George Roberts and Tony Gray KSC-2009-5968

CAPE CANAVERAL, Fla. – NASA's Ares I-X test rocket ignites its first s...

CAPE CANAVERAL, Fla. – NASA's Ares I-X test rocket ignites its first stage at Launch Pad 39B at NASA's Kennedy Space Center in Florida at 11:30 a.m. EDT on Oct. 28. The Constellation Program's 327-foot-tall roc... More

CAPE CANAVERAL, Fla. – The Ares I-X test rocket launches into a bright Florida sky from Launch Pad 39B at NASA's Kennedy Space Center in Florida at 11:30 a.m. EDT on Oct. 28. NASA’s Constellation Program's 327-foot-tall rocket produces 2.96 million pounds of thrust at liftoff and reaches a speed of 100 mph in eight seconds. This was the first launch from Kennedy's pads of a vehicle other than the space shuttle since the Apollo Program's Saturn rockets were retired. The parts used to make the Ares I-X booster flew on 30 different shuttle missions ranging from STS-29 in 1989 to STS-106 in 2000. The data returned from more than 700 sensors throughout the rocket will be used to refine the design of future launch vehicles and bring NASA one step closer to reaching its exploration goals. For information on the Ares I-X vehicle and flight test, visit http://www.nasa.gov/aresIX. Photo credit: NASA/George Roberts and Tom Farrar KSC-2009-5973

CAPE CANAVERAL, Fla. – The Ares I-X test rocket launches into a bright...

CAPE CANAVERAL, Fla. – The Ares I-X test rocket launches into a bright Florida sky from Launch Pad 39B at NASA's Kennedy Space Center in Florida at 11:30 a.m. EDT on Oct. 28. NASA’s Constellation Program's 327-... More

CAPE CANAVERAL, Fla. - With nearly 7 million pounds of thrust generated with the aid of twin solid rocket boosters, space shuttle Atlantis roars into the blue skies over Launch Pad 39A at NASA's Kennedy Space Center in Florida. Liftoff on its STS-129 mission came at 2:28 p.m. EST Nov. 16. Aboard are crew members Commander Charles O. Hobaugh; Pilot Barry E. Wilmore; and Mission Specialists Leland Melvin, Randy Bresnik, Mike Foreman and Robert L. Satcher Jr. On STS-129, the crew will deliver two ExPRESS Logistics Carriers to the International Space Station, the largest of the shuttle's cargo carriers, containing 15 spare pieces of equipment including two gyroscopes, two nitrogen tank assemblies, two pump modules, an ammonia tank assembly and a spare latching end effector for the station's robotic arm. Atlantis will return to Earth a station crew member, Nicole Stott, who has spent more than two months aboard the orbiting laboratory. STS-129 is slated to be the final space shuttle Expedition crew rotation flight. For information on the STS-129 mission and crew, visit http://www.nasa.gov/mission_pages/shuttle/shuttlemissions/sts129/index.html. Photo credit: NASA/Rusty Backer and Tom Farrar KSC-2009-6387

CAPE CANAVERAL, Fla. - With nearly 7 million pounds of thrust generate...

CAPE CANAVERAL, Fla. - With nearly 7 million pounds of thrust generated with the aid of twin solid rocket boosters, space shuttle Atlantis roars into the blue skies over Launch Pad 39A at NASA's Kennedy Space C... More

CAPE CANAVERAL, Fla. – Inside Orbiter Processing Facility-1 at NASA’s Kennedy Space Center in Florida, United Space Alliance technicians monitor the progress as a large crane lifts the right orbital maneuvering system, or OMS, pod for installation on space shuttle Atlantis. It is the last time an OMS pod will be installed on Atlantis. The OMS provided the shuttle with thrust for orbit insertion, rendezvous and deorbit, and could provide up to 1,000 pounds of propellant to the aft reaction control system. The OMS is housed in two independent pods located on each side of the shuttle’s aft fuselage. Each pod contains one OMS engine and the hardware needed to pressurize, store and distribute the propellants to perform the velocity maneuvers. Atlantis’ OMS pods were removed and sent to the test facility at White Sands Space Harbor in New Mexico to be cleaned of residual toxic propellant. The work is part of the Space Shuttle Program’s transition and retirement processing of the space shuttle fleet. A groundbreaking was held Jan. 18 for Atlantis’ future home, a 65,000-square-foot exhibit hall in Shuttle Plaza at the Kennedy Space Center Visitor Complex. Atlantis is scheduled to roll over to the visitor complex in November in preparation for the exhibit’s grand opening in July 2013. For more information, visit http://www.nasa.gov/transition. Photo credit: NASA/Dimitri Gerondidakis KSC-2012-3406

CAPE CANAVERAL, Fla. – Inside Orbiter Processing Facility-1 at NASA’s ...

CAPE CANAVERAL, Fla. – Inside Orbiter Processing Facility-1 at NASA’s Kennedy Space Center in Florida, United Space Alliance technicians monitor the progress as a large crane lifts the right orbital maneuverin... More

CAPE CANAVERAL, Fla. -- In the Vehicle Assembly Building at NASA’s Kennedy Space Center in Florida, technicians are documenting the installation of radius blocks to space shuttle Discovery's external fuel tank's support beams known as "stringers" near the intertank’s thrust panel area. The thrust panel is where the tank meets the two solid rocket boosters and sees the most stress during the flight into orbit. After the modifications and additional scans of the stringers are complete, foam insulation will be re-applied. Discovery's next launch opportunity to the International Space Station on the STS-133 mission is targeted for liftoff Feb. 24. For more information on STS-133, visit www.nasa.gov/mission_pages/shuttle/shuttlemissions/sts133/. Photo credit: NASA/Jack Pfaller KSC-2011-1072

CAPE CANAVERAL, Fla. -- In the Vehicle Assembly Building at NASA’s Ken...

CAPE CANAVERAL, Fla. -- In the Vehicle Assembly Building at NASA’s Kennedy Space Center in Florida, technicians are documenting the installation of radius blocks to space shuttle Discovery's external fuel tank'... More

CAPE CANAVERAL, Fla. – Inside Orbiter Processing Facility-1 at NASA’s Kennedy Space Center in Florida, United Launch Alliance technicians provide assistance as a large crane is lowered toward the right orbital maneuvering system, or OMS, pod for space shuttle Atlantis. It will be the last time an OMS pod is installed on Atlantis. The OMS provided the shuttle with thrust for orbit insertion, rendezvous and deorbit, and could provide up to 1,000 pounds of propellant to the aft reaction control system. The OMS is housed in two independent pods located on each side of the shuttle’s aft fuselage. Each pod contains one OMS engine and the hardware needed to pressurize, store and distribute the propellants to perform the velocity maneuvers. Atlantis’ OMS pods were removed and sent to the test facility at White Sands Space Harbor in New Mexico to be cleaned of residual toxic propellant. The work is part of the Space Shuttle Program’s transition and retirement processing of the space shuttle fleet. A groundbreaking was held Jan. 18 for Atlantis’ future home, a 65,000-square-foot exhibit hall in Shuttle Plaza at the Kennedy Space Center Visitor Complex. Atlantis is scheduled to roll over to the visitor complex in November in preparation for the exhibit’s grand opening in July 2013. For more information, visit http://www.nasa.gov/transition. Photo credit: NASA/Dimitri Gerondidakis KSC-2012-3400

CAPE CANAVERAL, Fla. – Inside Orbiter Processing Facility-1 at NASA’s ...

CAPE CANAVERAL, Fla. – Inside Orbiter Processing Facility-1 at NASA’s Kennedy Space Center in Florida, United Launch Alliance technicians provide assistance as a large crane is lowered toward the right orbital ... More

CAPE CANAVERAL, Fla. – At NASA’s Kennedy Space Center in Florida, a crane is used to load the aft skirt for a space shuttle solid rocket booster on a truck. A twin set of space shuttle solid rocket boosters and an external fuel tank are being prepared for transport to separate museums. The solid rocket boosters, or SRBs, will be displayed at the California Science Center in Los Angeles. The external tank soon will be transported for display at the Wings of Dreams Aviation Museum at Keystone Heights Airport between Gainesville and Jacksonville, Fla. The 149-foot SRBs together provided six million pounds of thrust. The external fuel tank contained over 500,000 gallons of liquid hydrogen and liquid oxygen propellant for the shuttle orbiters' three main engines. The work is part of Transition and Retirement of the space shuttle. For more information, visit http://www.nasa.gov/transition Photo credit: NASA/ Dimitri Gerondidakis KSC-2012-4455

CAPE CANAVERAL, Fla. – At NASA’s Kennedy Space Center in Florida, a cr...

CAPE CANAVERAL, Fla. – At NASA’s Kennedy Space Center in Florida, a crane is used to load the aft skirt for a space shuttle solid rocket booster on a truck. A twin set of space shuttle solid rocket boosters and... More

CAPE CANAVERAL, Fla. – At NASA’s Kennedy Space Center in Florida, a twin set of space shuttle solid rocket boosters and an external fuel tank are being loaded on trucks for transport to separate museums. The solid rocket boosters, or SRBs, will be displayed at the California Science Center in Los Angeles. The external tank soon will be transported for display at the Wings of Dreams Aviation Museum at Keystone Heights Airport between Gainesville and Jacksonville, Fla. The 149-foot SRBs together provided six million pounds of thrust. The external fuel tank contained over 500,000 gallons of liquid hydrogen and liquid oxygen propellant for the shuttle orbiters' three main engines. The work is part of Transition and Retirement of the space shuttle. For more information, visit http://www.nasa.gov/transition Photo credit: NASA/ Dimitri Gerondidakis KSC-2012-4446

CAPE CANAVERAL, Fla. – At NASA’s Kennedy Space Center in Florida, a tw...

CAPE CANAVERAL, Fla. – At NASA’s Kennedy Space Center in Florida, a twin set of space shuttle solid rocket boosters and an external fuel tank are being loaded on trucks for transport to separate museums. T... More

CAPE CANAVERAL, Fla. - With nearly 7 million pounds of thrust generated by twin solid rocket boosters and three main engines, space shuttle Atlantis clears the tower on Launch Pad 39A at NASA's Kennedy Space Center in Florida. Liftoff on its STS-129 mission came at 2:28 p.m. EST Nov. 16. Aboard are crew members Commander Charles O. Hobaugh; Pilot Barry E. Wilmore; and Mission Specialists Leland Melvin, Randy Bresnik, Mike Foreman and Robert L. Satcher Jr. On STS-129, the crew will deliver two ExPRESS Logistics Carriers to the International Space Station, the largest of the shuttle's cargo carriers, containing 15 spare pieces of equipment including two gyroscopes, two nitrogen tank assemblies, two pump modules, an ammonia tank assembly and a spare latching end effector for the station's robotic arm. Atlantis will return to Earth a station crew member, Nicole Stott, who has spent more than two months aboard the orbiting laboratory. STS-129 is slated to be the final space shuttle Expedition crew rotation flight. For information on the STS-129 mission and crew, visit http://www.nasa.gov/mission_pages/shuttle/shuttlemissions/sts129/index.html. Photo credit: NASA/Tom Farrar and Tony Gray KSC-2009-6392

CAPE CANAVERAL, Fla. - With nearly 7 million pounds of thrust generate...

CAPE CANAVERAL, Fla. - With nearly 7 million pounds of thrust generated by twin solid rocket boosters and three main engines, space shuttle Atlantis clears the tower on Launch Pad 39A at NASA's Kennedy Space Ce... More

KENNEDY SPACE CENTER, FLA. - In Orbiter Processing Facility Bay 1, technicians work on the Forward Reaction Control System (FRCS) of space shuttle Atlantis as it sits in the transfer aisle prior to installation. The FRCS provides the thrust for attitude (rotational) maneuvers (pitch, yaw and roll) and for small velocity changes along the orbiter axis (translation maneuvers). Processing of Atlantis is under way for mission STS-115, the 19th flight to the International Space Station. KSC-05pd2545

KENNEDY SPACE CENTER, FLA. - In Orbiter Processing Facility Bay 1, t...

KENNEDY SPACE CENTER, FLA. - In Orbiter Processing Facility Bay 1, technicians work on the Forward Reaction Control System (FRCS) of space shuttle Atlantis as it sits in the transfer aisle prior to installati... More

Saturn I - Saturn Apollo Program - Cluster of eight H-1 engines

Saturn I - Saturn Apollo Program - Cluster of eight H-1 engines

A Cluster of eight H-1 engines were used to thrust the first stage of Saturn I (S-I stage) and Saturn IB (S-IB stage). The engines were arranged in a double pattern. Four engines, located inboard, were fixed in... More

CAPE CANAVERAL, Fla. – In NASA Kennedy Space Center's Orbiter Processing Facility 2, workers remove the forward reaction control system, or FRCS, from space shuttle Endeavour's forward fuselage nose area. The FRCS provides the thrust for attitude (rotational) maneuvers (pitch, yaw and roll) and for small velocity changes along the orbiter axis (translation maneuvers). Endeavour is designated as the shuttle for the STS-130 mission, targeted for launch in February 2010. Photo credit: NASA/Jack Pfaller KSC-2009-4796

CAPE CANAVERAL, Fla. – In NASA Kennedy Space Center's Orbiter Processi...

CAPE CANAVERAL, Fla. – In NASA Kennedy Space Center's Orbiter Processing Facility 2, workers remove the forward reaction control system, or FRCS, from space shuttle Endeavour's forward fuselage nose area. The F... More

KENNEDY SPACE CENTER, FLA. - In the Space Shuttle Main Engine (SSME) Processing Facility, Boeing-Rocketdyne crane operator Joe Ferrante (left) lowers SSME 2058, the first SSME fully assembled at KSC, onto an engine stand with the assistance of other technicians on his team. The engine is being moved from its vertical work stand into a horizontal position in preparation for shipment to NASA’s Stennis Space Center in Mississippi to undergo a hot fire acceptance test. It is the first of five engines to be fully assembled on site to reach the desired number of 15 engines ready for launch at any given time in the Space Shuttle program. A Space Shuttle has three reusable main engines. Each is 14 feet long, weighs about 7,800 pounds, is seven-and-a-half feet in diameter at the end of its nozzle, and generates almost 400,000 pounds of thrust. Historically, SSMEs were assembled in Canoga Park, Calif., with post-flight inspections performed at KSC. Both functions were consolidated in February 2002. The Rocketdyne Propulsion and Power division of The Boeing Co. manufactures the engines for NASA. KSC-04pd1646

KENNEDY SPACE CENTER, FLA. - In the Space Shuttle Main Engine (SSME) P...

KENNEDY SPACE CENTER, FLA. - In the Space Shuttle Main Engine (SSME) Processing Facility, Boeing-Rocketdyne crane operator Joe Ferrante (left) lowers SSME 2058, the first SSME fully assembled at KSC, onto an en... More

CAPE CANAVERAL, Fla. – Inside Orbiter Processing Facility-1 at NASA’s Kennedy Space Center in Florida, preparations are underway to install the right orbital maneuvering system, or OMS, pod on space shuttle Atlantis. It will be the last time an OMS pod is installed on Atlantis. The OMS provided the shuttle with thrust for orbit insertion, rendezvous and deorbit, and could provide up to 1,000 pounds of propellant to the aft reaction control system. The OMS is housed in two independent pods located on each side of the shuttle’s aft fuselage. Each pod contains one OMS engine and the hardware needed to pressurize, store and distribute the propellants to perform the velocity maneuvers. Atlantis’ OMS pods were removed and sent to the test facility at White Sands Space Harbor in New Mexico to be cleaned of residual toxic propellant. The work is part of the Space Shuttle Program’s transition and retirement processing of the space shuttle fleet. A groundbreaking was held Jan. 18 for Atlantis’ future home, a 65,000-square-foot exhibit hall in Shuttle Plaza at the Kennedy Space Center Visitor Complex. Atlantis is scheduled to roll over to the visitor complex in November in preparation for the exhibit’s grand opening in July 2013. For more information, visit http://www.nasa.gov/transition. Photo credit: NASA/Dimitri Gerondidakis KSC-2012-3398

CAPE CANAVERAL, Fla. – Inside Orbiter Processing Facility-1 at NASA’s ...

CAPE CANAVERAL, Fla. – Inside Orbiter Processing Facility-1 at NASA’s Kennedy Space Center in Florida, preparations are underway to install the right orbital maneuvering system, or OMS, pod on space shuttle At... More

CAPE CANAVERAL, Fla. – Inside Orbiter Processing Facility-1 at NASA’s Kennedy Space Center in Florida, the left orbital maneuvering system, or OMS, pod has been installed onto space shuttle Atlantis. The OMS provided the shuttle with thrust for orbit insertion, rendezvous and deorbit, and could provide up to 1,000 pounds of propellant to the aft reaction control system. The OMS is housed in two independent pods located on each side of the shuttle’s aft fuselage. Each pod contains one OMS engine and the hardware needed to pressurize, store and distribute the propellants to perform the velocity maneuvers. Atlantis’ OMS pods were removed and sent to White Sands Test Facility in New Mexico to be cleaned of residual toxic propellant. The work is part of the Space Shuttle Program’s transition and retirement processing of the space shuttle fleet. A groundbreaking was held Jan. 18 for Atlantis’ future home, a 65,000-square-foot exhibit hall in Shuttle Plaza at the Kennedy Space Center Visitor Complex. Atlantis is scheduled to roll over to the visitor complex in November in preparation for the exhibit’s grand opening in July 2013. For more information, visit http://www.nasa.gov/transition. Photo credit: NASA/Ben Smegelsky KSC-2012-3351

CAPE CANAVERAL, Fla. – Inside Orbiter Processing Facility-1 at NASA’s ...

CAPE CANAVERAL, Fla. – Inside Orbiter Processing Facility-1 at NASA’s Kennedy Space Center in Florida, the left orbital maneuvering system, or OMS, pod has been installed onto space shuttle Atlantis. The OMS pr... More

CAPE CANAVERAL, Fla. - At NASA's Kennedy Space Center in Florida, the Forward Reaction Control System, or FRCS, for space shuttle Discovery arrives at Orbiter Processing Facility Bay 3. Discovery is being prepared for the STS-131 mission, the 33rd flight to the International Space Station. The FRCS provides the thrust for attitude (rotational) maneuvers (pitch, yaw and roll) and for small velocity changes along the orbiter axis (translation maneuvers). The seven-member STS-131 crew will deliver a Multi-Purpose Logistics Module filled with resupply stowage platforms and racks to be transferred to locations around the station. Three spacewalks will include work to attach a spare ammonia tank assembly to the station's exterior and return a European experiment from outside the station's Columbus module. Discovery's launch is targeted for March 18, 2010. For information on the STS-131 mission and crew, visit http://www.nasa.gov/mission_pages/shuttle/shuttlemissions/sts131/index.html. Photo credit: NASA/Jack Pfaller KSC-2009-6706

CAPE CANAVERAL, Fla. - At NASA's Kennedy Space Center in Florida, the ...

CAPE CANAVERAL, Fla. - At NASA's Kennedy Space Center in Florida, the Forward Reaction Control System, or FRCS, for space shuttle Discovery arrives at Orbiter Processing Facility Bay 3. Discovery is being pr... More

CAPE CANAVERAL, Fla. - With more than 23 times the power output of the Hoover Dam, NASA’s Ares I-X test rocket soars into blue skies above Launch Pad 39B at NASA's Kennedy Space Center in Florida. The rocket produces 2.96 million pounds of thrust at liftoff and reaches a speed of 100 mph in eight seconds. Liftoff of the 6-minute flight test was at 11:30 a.m. EDT Oct. 28. This was the first launch from Kennedy's pads of a vehicle other than the space shuttle since the Apollo Program's Saturn rockets were retired. The parts used to make the Ares I-X booster flew on 30 different shuttle missions ranging from STS-29 in 1989 to STS-106 in 2000. The data returned from more than 700 sensors throughout the rocket will be used to refine the design of future launch vehicles and bring NASA one step closer to reaching its exploration goals. For information on the Ares I-X vehicle and flight test, visit http://www.nasa.gov/aresIX. Photo credit: NASA/Sandra Joseph and Kevin O'Connel KSC-2009-6008

CAPE CANAVERAL, Fla. - With more than 23 times the power output of the...

CAPE CANAVERAL, Fla. - With more than 23 times the power output of the Hoover Dam, NASA’s Ares I-X test rocket soars into blue skies above Launch Pad 39B at NASA's Kennedy Space Center in Florida. The rocket p... More

The static firing of a Saturn F-1 engine at the Marshall Space Flight Center's Static Test Stand. The F-1 engine is a single-start, 1,5000,000 Lb fixed-thrust, bipropellant rocket system. The engine uses liquid oxygen as the oxidizer and RP-1 (kerosene) as fuel. The five-engine cluster used on the first stage of the Saturn V produces 7,500,000 lbs of thrust. n/a

The static firing of a Saturn F-1 engine at the Marshall Space Flight ...

The static firing of a Saturn F-1 engine at the Marshall Space Flight Center's Static Test Stand. The F-1 engine is a single-start, 1,5000,000 Lb fixed-thrust, bipropellant rocket system. The engine uses liqui... More

Saturn I launch vehicle - Saturn Apollo Program

Saturn I launch vehicle - Saturn Apollo Program

A completed Saturn I launch vehicle in the Fabrication and Assembly Engineering Division at the Marshall Space Flight Center. The Saturn I launch vehicle is composed of an S-I first stage or booster (rear), pow... More

Saturn Apollo Program. NASA public domain image colelction.

Saturn Apollo Program. NASA public domain image colelction.

On October 27, 1961, the Marshall Space Flight Center (MSFC) and the Nation marked a high point in the 3-year-old Saturn development program when the first Saturn vehicle flew a flawless 215-mile ballistic traj... More

At its founding, the Marshall Space Flight Center (MSFC) inherited the Army’s Jupiter and Redstone test stands, but much larger facilities were needed for the giant stages of the Saturn V. From 1960 to 1964, the existing stands were remodeled and a sizable new test area was developed. The new comprehensive test complex for propulsion and structural dynamics was unique within the nation and the free world, and they remain so today because they were constructed with foresight to meet the future as well as on going needs. Construction of the S-IC Static test stand complex began in 1961 in the west test area of MSFC, and was completed in 1964. The S-IC static test stand was designed to develop and test the 138-ft long and 33-ft diameter Saturn V S-IC first stage, or booster stage, weighing in at 280,000 pounds. Required to hold down the brute force of a 7,500,000-pound thrust produced by 5 F-1 engines, the S-IC static test stand was designed and constructed with the strength of hundreds of tons of steel and 12,000,000 pounds of cement, planted down to bedrock 40 feet below ground level. The foundation walls, constructed with concrete and steel, are 4 feet thick. The base structure consists of four towers with 40-foot-thick walls extending upward 144 feet above ground level. The structure was topped by a crane with a 135-foot boom. With the boom in the upright position, the stand was given an overall height of 405 feet, placing it among the highest structures in Alabama at the time. Construction of the S-IC test stand came to a halt at the end of September as the determination was made that the Saturn booster size had to be increased. As a result, the stand had to be modified. With construction delayed, and pumps turned off, this photo, taken December 11, 1961, shows the abandoned site with floods above the 18 ft mark. The flooding was caused by the disturbance of a natural spring months prior during the excavation of the site. n/a

At its founding, the Marshall Space Flight Center (MSFC) inherited the...

At its founding, the Marshall Space Flight Center (MSFC) inherited the Army’s Jupiter and Redstone test stands, but much larger facilities were needed for the giant stages of the Saturn V. From 1960 to 1964, th... More

Saturn Apollo Program, Apollo program Saturn V rocket images

Saturn Apollo Program, Apollo program Saturn V rocket images

This photograph depicts the Rocketdyne static firing of the F-1 engine at the towering 76-meter Test Stand 1-C in Area 1-125 of the Edwards Air Force Base in California. The Saturn V S-IC (first) stage utilized... More

At its founding, the Marshall Space Flight Center (MSFC) inherited the Army’s Jupiter and Redstone test stands, but much larger facilities were needed for the giant stages of the Saturn V. From 1960 to 1964, the existing stands were remodeled and a sizable new test area was developed. The new comprehensive test complex for propulsion and structural dynamics was unique within the nation and the free world, and they remain so today because they were constructed with foresight to meet the future as well as on going needs. Construction of the S-IC Static test stand complex began in 1961 in the west test area of MSFC, and was completed in 1964. The S-IC static test stand was designed to develop and test the 138-ft long and 33-ft diameter Saturn V S-IC first stage, or booster stage, weighing in at 280,000 pounds. Required to hold down the brute force of a 7,500,000-pound thrust produced by 5 F-1 engines, the S-IC static test stand was designed and constructed with the strength of hundreds of tons of steel and 12,000,000 pounds of cement, planted down to bedrock 40 feet below ground level. The foundation walls, constructed with concrete and steel, are 4 feet thick. The base structure consists of four towers with 40-foot-thick walls extending upward 144 feet above ground level. The structure was topped by a crane with a 135-foot boom. With the boom in the upright position, the stand was given an overall height of 405 feet, placing it among the highest structures in Alabama at the time. In addition to the S-IC test stand, related facilities were built during this time. Built to the north of the massive S-IC test stand, was the F-1 Engine test stand. The F-1 test stand, a vertical engine firing test stand, 239 feet in elevation and 4,600 square feet in area at the base, was designed to assist in the development of the F-1 Engine. Capability was provided for static firing of 1.5 million pounds of thrust using liquid oxygen and kerosene. Like the S-IC stand, the foundation of the F-1 stand is keyed into the bedrock approximately 40 feet below grade. This photo, taken October 26, 1962, depicts the excavation process of the single engine F-1 stand. n/a

At its founding, the Marshall Space Flight Center (MSFC) inherited the...

At its founding, the Marshall Space Flight Center (MSFC) inherited the Army’s Jupiter and Redstone test stands, but much larger facilities were needed for the giant stages of the Saturn V. From 1960 to 1964, th... More

At its founding, the Marshall Space Flight Center (MSFC) inherited the Army’s Jupiter and Redstone test stands, but much larger facilities were needed for the giant stages of the Saturn V. From 1960 to 1964, the existing stands were remodeled and a sizable new test area was developed. The new comprehensive test complex for propulsion and structural dynamics was unique within the nation and the free world, and they remain so today because they were constructed with foresight to meet the future as well as on going needs. Construction of the S-IC Static test stand complex began in 1961 in the west test area of MSFC, and was completed in 1964. The S-IC static test stand was designed to develop and test the 138-ft long and 33-ft diameter Saturn V S-IC first stage, or booster stage, weighing in at 280,000 pounds. Required to hold down the brute force of a 7,500,000-pound thrust produced by 5 F-1 engines, the S-IC static test stand was designed and constructed with the strength of hundreds of tons of steel and 12,000,000 pounds of cement, planted down to bedrock 40 feet below ground level. The foundation walls, constructed with concrete and steel, are 4 feet thick. The base structure consists of four towers with 40-foot-thick walls extending upward 144 feet above ground level. The structure was topped by a crane with a 135-foot boom. With the boom in the upright position, the stand was given an overall height of 405 feet, placing it among the highest structures in Alabama at the time. In addition to the S-IC test stand, related facilities were built during this time. Built to the north of the massive S-IC test stand, was the F-1 Engine test stand. The F-1 test stand, a vertical engine firing test stand, 239 feet in elevation and 4,600 square feet in area at the base, was designed to assist in the development of the F-1 Engine. Capability was provided for static firing of 1.5 million pounds of thrust using liquid oxygen and kerosene. Like the S-IC stand, the foundation of the F-1 stand is keyed into the bedrock approximately 40 feet below grade. This photo, taken November 15, 1962, depicts the excavation process of the single engine F-1 stand site. n/a

At its founding, the Marshall Space Flight Center (MSFC) inherited the...

At its founding, the Marshall Space Flight Center (MSFC) inherited the Army’s Jupiter and Redstone test stands, but much larger facilities were needed for the giant stages of the Saturn V. From 1960 to 1964, th... More

Saturn I - Saturn Apollo Program

Saturn I - Saturn Apollo Program

The Saturn I (SA-3) flight lifted off from Kennedy Space Center launch Complex 34, November 16, 1962. The third launch of Saturn launch vehicles, developed at the Marshall Space Flight Center (MSFC) under the d... More

Saturn V F-1 Engine - Saturn Apollo Program

Saturn V F-1 Engine - Saturn Apollo Program

A close-up view of the F-1 Engine for the Saturn V S-IC (first) stage depicts the complexity of the engine. Developed by Rocketdyne under the direction of the Marshall Space Flight Center, the F-1 engine was ut... More

Marshall Space Center construction progress

Marshall Space Center construction progress

At its founding, the Marshall Space Flight Center (MSFC) inherited the Army’s Jupiter and Redstone test stands, but much larger facilities were needed for the giant stages of the Saturn V. From 1960 to 1964, th... More

At its founding, the Marshall Space Flight Center (MSFC) inherited the Army’s Jupiter and Redstone test stands, but much larger facilities were needed for the giant stages of the Saturn V. From 1960 to 1964, the existing stands were remodeled and a sizable new test area was developed. The new comprehensive test complex for propulsion and structural dynamics was unique within the nation and the free world, and they remain so today because they were constructed with foresight to meet the future as well as on going needs. Construction of the S-IC Static test stand complex began in 1961 in the west test area of MSFC, and was completed in 1964. The S-IC static test stand was designed to develop and test the 138-ft long and 33-ft diameter Saturn V S-IC first stage, or booster stage, weighing in at 280,000 pounds. Required to hold down the brute force of a 7,500,000-pound thrust produced by 5 F-1 engines, the S-IC static test stand was designed and constructed with the strength of hundreds of tons of steel and 12,000,000 pounds of cement, planted down to bedrock 40 feet below ground level. The foundation walls, constructed with concrete and steel, are 4 feet thick. The base structure consists of four towers with 40-foot-thick walls extending upward 144 feet above ground level. The structure was topped by a crane with a 135-foot boom. With the boom in the upright position, the stand was given an overall height of 405 feet, placing it among the highest structures in Alabama at the time. In addition to the stand itself, related facilities were constructed during this time. Built directly east of the test stand was the Block House, which served as the control center for the test stand. The two were connected by a narrow access tunnel which housed the cables for the controls. The F-1 Engine test stand was built north of the massive S-IC test stand. The F-1 test stand is a vertical engine firing test stand, 239 feet in elevation and 4,600 square feet in area at the base, and was designed to assist in the development of the F-1 Engine. Capability is provided for static firing of 1.5 million pounds of thrust using liquid oxygen and kerosene. Like the S-IC stand, the foundation of the F-1 stand is keyed into the bedrock approximately 40 feet below grade. This aerial photograph, taken January 15, 1963 gives an overall view of the construction progress of the newly developed test complex. The large white building located in the center is the Block House. Just below and to the right of it is the S-IC test stand. The large hole to the left of the S-IC stand is the F-1 test stand site. n/a

At its founding, the Marshall Space Flight Center (MSFC) inherited the...

At its founding, the Marshall Space Flight Center (MSFC) inherited the Army’s Jupiter and Redstone test stands, but much larger facilities were needed for the giant stages of the Saturn V. From 1960 to 1964, th... More

At its founding, the Marshall Space Flight Center (MSFC) inherited the Army’s Jupiter and Redstone test stands, but much larger facilities were needed for the giant stages of the Saturn V. From 1960 to 1964, the existing stands were remodeled and a sizable new test area was developed. The new comprehensive test complex for propulsion and structural dynamics was unique within the nation and the free world, and they remain so today because they were constructed with foresight to meet the future as well as on going needs. Construction of the S-IC Static test stand complex began in 1961 in the west test area of MSFC, and was completed in 1964. The S-IC static test stand was designed to develop and test the 138-ft long and 33-ft diameter Saturn V S-IC first stage, or booster stage, weighing in at 280,000 pounds. Required to hold down the brute force of a 7,500,000-pound thrust produced by 5 F-1 engines, the S-IC static test stand was designed and constructed with the strength of hundreds of tons of steel and 12,000,000 pounds of cement, planted down to bedrock 40 feet below ground level. The foundation walls, constructed with concrete and steel, are 4 feet thick. The base structure consists of four towers with 40-foot-thick walls extending upward 144 feet above ground level. The structure was topped by a crane with a 135-foot boom. With the boom in the upright position, the stand was given an overall height of 405 feet, placing it among the highest structures in Alabama at the time. In addition to the stand itself, related facilities were constructed during this time. Built directly east of the test stand was the Block House, which served as the control center for the test stand. The two were connected by a narrow access tunnel which housed the cables for the controls. The F-1 Engine test stand was built north of the massive S-IC test stand. The F-1 test stand is a vertical engine firing test stand, 239 feet in elevation and 4,600 square feet in area at the base, and was designed to assist in the development of the F-1 Engine. Capability is provided for static firing of 1.5 million pounds of thrust using liquid oxygen and kerosene. Like the S-IC stand, the foundation of the F-1 stand is keyed into the bedrock approximately 40 feet below grade. This aerial photograph, taken January 15, 1963, gives a close overall view of the newly developed test complex. Depicted in the forefront center is the S-IC test stand with towers prominent, the Block House is seen in the center just above the S-IC test stand, and the large hole to the left, located midway between the two is the F-1 test stand site. n/a

At its founding, the Marshall Space Flight Center (MSFC) inherited the...

At its founding, the Marshall Space Flight Center (MSFC) inherited the Army’s Jupiter and Redstone test stands, but much larger facilities were needed for the giant stages of the Saturn V. From 1960 to 1964, th... More

Saturn Apollo Program - working on a mock up of the S-IC thrust structure

Saturn Apollo Program - working on a mock up of the S-IC thrust struct...

This photograph depicts Marshall Space Flight Center employees, James Reagin, machinist (top); Floyd McGinnis, machinist; and Ernest Davis, experimental test mechanic (foreground), working on a mock up of the S... More

The Saturn I (SA-4) flight lifted off from Kennedy Space Center launch Complex 34, March 28, 1963. The fourth launch of Saturn launch vehicles, developed at the Marshall Space Flight Center (MSFC) under the direction of Dr. Wernher von Braun, incorporated a Saturn I, Block I engine. The typical height of a Block I vehicle was approximately 163 feet and had only one live stage. It consisted of eight tanks, each 70 inches in diameter, clustered around a central tank, 105 inches in diameter. Four of the external tanks were fuel tanks for the RP-1 (kerosene) fuel. The other four, spaced alternately with the fuel tanks, were liquid oxygen tanks as was the large center tank. All fuel tanks and liquid oxygen tanks drained at the same rates respectively. The thrust for the stage came from eight H-1 engines, each producing a thrust of 165,000 pounds, for a total thrust of over 1,300,000 pounds. The engines were arranged in a double pattern. Four engines, located inboard, were fixed in a square pattern around the stage axis and canted outward slightly, while the remaining four engines were located outboard in a larger square pattern offset 40 degrees from the inner pattern. Unlike the inner engines, each outer engine was gimbaled. That is, each could be swung through an arc. They were gimbaled as a means of steering the rocket, by letting the instrumentation of the rocket correct any deviations of its powered trajectory. The block I required engine gimabling as the only method of guiding and stabilizing the rocket through the lower atmosphere. The upper stages of the Block I rocket reflected the three-stage configuration of the Saturn I vehicle. Like SA-3, the SA-4 flight’s upper stage ejected 113,560 liters (30,000 gallons) of ballast water in the upper atmosphere for "Project Highwater" physics experiment. Release of this vast quantity of water in a near-space environment marked the second purely scientific large-scale experiment. The SA-4 was the last Block I rocket launch. n/a

The Saturn I (SA-4) flight lifted off from Kennedy Space Center launch...

The Saturn I (SA-4) flight lifted off from Kennedy Space Center launch Complex 34, March 28, 1963. The fourth launch of Saturn launch vehicles, developed at the Marshall Space Flight Center (MSFC) under the dir... More

The Saturn I (SA-4) flight lifted off from Kennedy Space Center launch Complex 34, March 28, 1963. The fourth launch of Saturn launch vehicles developed at the Marshall Space Flight Center (MSFC), under the direction of Dr. Wernher von Braun, incorporated a Saturn I, Block I engine. The typical height of a Block I vehicle was approximately 163 feet and had only one live stage. It consisted of eight tanks, each 70 inches in diameter, clustered around a central tank, 105 inches in diameter. Four of the external tanks were fuel tanks for the RP-1 (kerosene) fuel. The other four, spaced alternately with the fuel tanks, were liquid oxygen tanks as was the large center tank. All fuel tanks and liquid oxygen tanks drained at the same rates respectively. The thrust for the stage came from eight H-1 engines, each producing a thrust of 165,000 pounds, for a total thrust of over 1,300,000 pounds. The engines were arranged in a double pattern. Four engines, located inboard, were fixed in a square pattern around the stage axis and canted outward slightly, while the remaining four engines were located outboard in a larger square pattern offset 40 degrees from the inner pattern. Unlike the inner engines, each outer engine was gimbaled. That is, each could be swung through an arc. They were gimbaled as a means of steering the rocket, by letting the instrumentation of the rocket correct any deviations of its powered trajectory. The block I required engine gimabling as the only method of guiding and stabilizing the rocket through the lower atmosphere. The upper stages of the Block I rocket reflected the three-stage configuration of the Saturn I vehicle. Like SA-3, the SA-4 flight’s upper stage ejected 113,560 liters (30,000 gallons) of ballast water in the upper atmosphere for "Project Highwater" physics experiment. Release of this vast quantity of water in a near-space environment marked the second purely scientific large-scale experiment. The SA-4 was the last Block I rocket launch. n/a

The Saturn I (SA-4) flight lifted off from Kennedy Space Center launch...

The Saturn I (SA-4) flight lifted off from Kennedy Space Center launch Complex 34, March 28, 1963. The fourth launch of Saturn launch vehicles developed at the Marshall Space Flight Center (MSFC), under the dir... More

Full scale engineering mock-up of Saturn V - Saturn Apollo Program

Full scale engineering mock-up of Saturn V - Saturn Apollo Program

This image illustrates technicians working on a full scale engineering mock-up of a Saturn V S-IC stage thrust structure nearing completion at the Manufacturing Engineering Laboratory at Marshall Space Flight C... More

Marshall Space Center construction progress

Marshall Space Center construction progress

At its founding, the Marshall Space Flight Center (MSFC) inherited the Army’s Jupiter and Redstone test stands, but much larger facilities were needed for the giant stages of the Saturn V. From 1960 to 1964, th... More

Marshall Space Center construction progress

Marshall Space Center construction progress

At its founding, the Marshall Space Flight Center (MSFC) inherited the Army’s Jupiter and Redstone test stands, but much larger facilities were needed for the giant stages of the Saturn V. From 1960 to 1964, th... More

Saturn V - Saturn Apollo Program

Saturn V - Saturn Apollo Program

This close-up view of the F-1 engine for the Saturn V S-IC (first) stage shows the engine's complexity, and also its large size as it dwarfs the technician. Developed by Rocketdyne, under the direction of the M... More

Diagrams of Spacecraft Responses to Orbit Attitude Control Thrust

Diagrams of Spacecraft Responses to Orbit Attitude Control Thrust

S64-03507 (1964) --- Diagrams shows Gemini spacecraft responses to orbital attitude systems's thrusters. Firing of appropriate combination of the thrusters cause pitch, roll and yaw.

The launch of the SA-5 - Saturn I - Saturn Apollo Program

The launch of the SA-5 - Saturn I - Saturn Apollo Program

Developed at MSFC under the direction of Dr. Wernher von Braun, the SA-5 incorporated a Saturn I, Block II engine. Launched on January 29, 1964, SA-5 was the first two stage (Block II) Saturn with orbital capab... More

Saturn I second stage - Saturn Apollo Program

Saturn I second stage - Saturn Apollo Program

The Saturn I S-IV stage (second stage) for the SA-7 mission being prepared for shipment to Cape Canaveral, Florida. The S-IV stage had six RL-10 engines, which used liquid hydrogen and liquid oxygen as its prop... More

The Saturn I S-IV stage (second stage) assembly

The Saturn I S-IV stage (second stage) assembly

The Saturn I S-IV stage (second stage) assembly for the SA-9 mission underwent the weight and balance test in the hanger building at Cape Canaveral. The S-IV stage had six RL-10 engines which used liquid hydrog... More

Saturn V S-IC-T stage (S-IC static test article) fuel tank

Saturn V S-IC-T stage (S-IC static test article) fuel tank

This image shows the Saturn V S-IC-T stage (S-IC static test article) fuel tank being attached to the thrust structure in the vehicle assembly building at the Marshall Space Flight Center (MSFC). The S-IC stage... More

Saturn V fuel tank assembly - Saturn Apollo Program

Saturn V fuel tank assembly - Saturn Apollo Program

At the Marshall Space Flight Center (MSFC), the fuel tank assembly for the Saturn V S-IC-T (static test stage) fuel tank assembly is mated to the liquid oxygen (LOX) tank in building 4705. This stage underwent ... More

Lunar Landing Research Vehicle in Flight

Lunar Landing Research Vehicle in Flight

(1965) In this 1965 NASA Flight Research Center photograph the Lunar Landing Research Vehicle (LLRV) is shown at near maximum altitude over the south base at Edwards Air Force Base. Built of tubular aluminum li... More

Lunar Landing Research Vehicle (LLRV) in flight

Lunar Landing Research Vehicle (LLRV) in flight

(1965) In this 1965 NASA Flight Research Center photograph the Lunar Landing Research Vehicle (LLRV) is shown at near maximum altitude over the south base at Edwards Air Force Base. Built of tubular aluminum li... More

Saturn V F-I engine - Saturn Apollo Program

Saturn V F-I engine - Saturn Apollo Program

Engineers and technicians at the Marshall Space Flight Center were installing an F-I engine on the Saturn V S-IC (first) stage thrust structure in building 4705. The S-IC (first) stage used five F-1 engines tha... More

Saturn V static testing stage - Saturn Apollo Program

Saturn V static testing stage - Saturn Apollo Program

Pictured is the Saturn V S-IC-T stage (static testing stage) being assembled in the horizontal assembly station at the Marshall Space Flight Center (MSFC), building 4705. This stage underwent numerous static fi... More

Saturn V S-IC-T stage - Saturn Apollo Program

Saturn V S-IC-T stage - Saturn Apollo Program

The S-IC-T stage was hoisted into the S-IC Static Test Stand at the Marshall Space Flight Center. The S-IC-T stage was a static test vehicle, not intended for flight. It was ground tested repeatedly over a peri... More

Saturn V F-1 engines - Saturn Apollo Program

Saturn V F-1 engines - Saturn Apollo Program

Engineers at the Marshall Space Flight Center install the F-1 engines on the S-IC stage thrust structure at the S-IC static test stand. Engines are installed on the stage after it has been placed in the test st... More

Saturn V F-1 engines - Saturn Apollo Program

Saturn V F-1 engines - Saturn Apollo Program

Engineers at the Marshall Space Flight Center install the F-1 engines on the S-IC stage thrust structure at the S-IC static test stand. Engines are installed on the stage after it has been placed in the test st... More

Saturn V S-IC static test stand - Saturn Apollo Program

Saturn V S-IC static test stand - Saturn Apollo Program

The S-IC-T stage was hoisted into the S-IC static test stand at the Marshall Space Flight Center. The S-IC-T stage was a static test vehicle not intended for flight. It was ground tested repeatedly over a perio... More

Saturn V - Saturn Apollo Program

Saturn V - Saturn Apollo Program

Engineers at the Marshall Space Flight Center install the F-1 engines on the S-IC stage thrust structure at the S-IC static test stand. Engines are installed on the stage after it has been placed in the test st... More

Saturn V F-1 engines - Saturn Apollo Program

Saturn V F-1 engines - Saturn Apollo Program

This photograph shows F-1 engines being stored in the F-1 Engine Preparation Shop, building 4666, at the Marshall Space Flight Center. Each F-1 engine produced a thrust of 1,500,000 pounds. A cluster of five en... More

Saturn V - S-IC-T stage is hoisted into the S-IC static test stand

Saturn V - S-IC-T stage is hoisted into the S-IC static test stand

The S-IC-T stage is hoisted into the S-IC static test stand at the Marshall Space Flight Center. The S-IC-T stage is a static test vehicle not intended for flight. It was ground tested repeatedly over a period ... More

Saturn V - S-IC-T stage (static firing stage)

Saturn V - S-IC-T stage (static firing stage)

The S-IC-T stage (static firing stage) is installed and awaits the first static firing of all five F-1 engines at the Marshall Space Flight Center S-IC static test stand. Constructed in 1964, the S-IC static te... More

Saturn V - the first test firing of all five F-1 engines

Saturn V - the first test firing of all five F-1 engines

This photograph depicts a dramatic view of the first test firing of all five F-1 engines for the Saturn V S-IC stage at the Marshall Space Flight Center. The testing lasted a full duration of 6.5 seconds. It al... More

Saturn Apollo Program - test firing of all five F-1 engines for the Saturn V

Saturn Apollo Program - test firing of all five F-1 engines for the Sa...

This photograph depicts a view of the test firing of all five F-1 engines for the Saturn V S-IC test stage at the Marshall Space Flight Center. The S-IC stage is the first stage, or booster, of a 364-foot long ... More

CAPE KENNEDY, Fla. -- At Cape Kennedy Air Force Station in Florida, a thrust augmented improved Delta lifts off with a three hundred eighty five pound geodetic Explorer spacecraft, designated GEOS-A. The spacecraft contains five geodetic instrumentation systems to provide simultaneous measurements that scientists require to establish a more precise model of the Earth's gravitational field, and to map a world coordinate system relating points on, or near the surface to the common center of mass. This will be the first launch for the improved Delta second stage. Photo Credit: NASA KSC-65P-0205

CAPE KENNEDY, Fla. -- At Cape Kennedy Air Force Station in Florida, a ...

CAPE KENNEDY, Fla. -- At Cape Kennedy Air Force Station in Florida, a thrust augmented improved Delta lifts off with a three hundred eighty five pound geodetic Explorer spacecraft, designated GEOS-A. The spacec... More

Saturn V launch vehicle. NASA Skylab space station

Saturn V launch vehicle. NASA Skylab space station

This is a cutaway illustration of the Saturn V launch vehicle with callouts of the major components. The Saturn V is the largest and most powerful launch vehicle developed in the United States. It was a three s... More

J-2 engine and the S-IVB (second) stage thrust structure

J-2 engine and the S-IVB (second) stage thrust structure

Workmen secure a J-2 engine onto the S-IVB (second) stage thrust structure. As part of Marshall Space Center's "building block" approach to the Saturn development, the S-IVB was utilized in the Saturn IBC launc... More

Saturn Apollo Program - firing of all five F-1 engines for the Saturn V S-IC test stage

Saturn Apollo Program - firing of all five F-1 engines for the Saturn ...

This photograph depicts a view of the test firing of all five F-1 engines for the Saturn V S-IC test stage at the Marshall Space Flight Center. The S-IC stage is the first stage, or booster, of a 364-foot long ... More

Previous

of 11

Next