Tag Archives: Manned Space Flight

20 February 1962, 14:47:39 UTC, T + 4 seconds

Launch of Friendship 7 from Launch Complex 14, Kennedy Space Center, 14:47:39 UTC, 20 February 1962. (NASA)

20 February 1962, 14:47:39 UTC: At 9:47:39 a.m., Eastern Standard Time, NASA’s Mercury-Atlas 6 lifted off from Launch Complex 14, Cape Canaveral Air Force Station, Cape Canaveral, Florida. This was the third launch of a manned Mercury spacecraft, and the first time that an Atlas rocket had been used.

Aboard the spacecraft was Lieutenant Colonel John Herschel Glenn, Jr., United States Marine Corps, an experienced fighter pilot and test pilot.

John Herschel Glenn, Jr., NASA Project Mercury Astronaut. (Ralph Morse/LIFE Magazine)

2 minutes, 10 seconds after liftoff, the booster engines cut of and were jettisoned. 23 seconds later, the escape tower, no longer needed, was also jettisoned. The Atlas sustainer engine continued to burn until T+00:05:20. The spacecraft had now reached 17,544 miles per hour (28,234 kilometers per hour) and was in an elliptical orbit around the Earth. At T+00:05:24 the Mercury spacecraft separated from the Atlas booster.

Glenn’s orbit had an apogee of 162.2 statute miles (261 kilometers) and perigee of 100 miles (161 kilometers). The orbit was inclined 32.54° relative to Earth’s orbital plane. Friendship 7 completed an orbit every 88 minutes, 29 seconds.

Analysis showed that the Atlas had placed Friendship 7 in orbit at a velocity with 7 feet per second (2.1 meters per second) less than nominal. However, computer analysis showed that the orbital trajectory was good enough for nearly 100 orbits.

This photograph of Friendship 7’s cockpit was taken in orbit around the Earth, 20 February 1962. Astronaut John Glenn’s hands and legs are visible at the lower edge of the image. (Ohio State University)

During the 4 hour, 55 minute, 23 second flight, the Mercury capsule orbited the Earth three times. John Glenn was the first American astronaut to orbit the Earth.  (Cosmonaut Yuri Gagarin had orbited the Earth 12 April 1961.)

After re-entry, the capsule parachuted into the Atlantic Ocean, only six miles from the recovery ship, USS Noa (DD-841).

The Mercury spacecraft, Friendship 7, was built by McDonnell Aircraft Corporation, St. Louis, Missouri. It was the 13th Mercury capsule built. Designed to carry one pilot, it could be controlled in pitch, roll and yaw by steam thrusters fueled by hydrogen peroxide. The Mercury was 9 feet, 7.72 inches (2.939 meters) long, conical, and had a maximum diameter of 6 feet, 2½ inches (1.885 meters). The spacecraft weighed 2,700 pounds (1,224.7 kilograms) at launch.

The rocket, a “1-½ stage” liquid-fueled Atlas LV-3B, number 109-D, was built by the  Convair Division of General Dynamics at San Diego, California. It was developed from a U.S. Air Force SM-65 Atlas D intercontinental ballistic missile, modified for use as a “man-rated” orbital launch vehicle.

The LV-3B was 65 feet (19.812 meters) long from the base to the Mercury adapter section, and the tank section is 10 feet (3.038 meters) in diameter. The complete Mercury-Atlas orbital launch vehicle is 93 feet (28.436 meters) tall, including the escape tower. When ready for launch it weighed approximately 260,000 pounds (118,000 kilograms) and could place a 3,000 pound (1,360 kilogram) payload into low Earth orbit.

The Atlas’ three engines were built by the Rocketdyne Division of North American Aviation, Inc., at Canoga Park, California. Two Rocketdyne LR89-NA-5 engines and one LR105-NA-5 produced 341,140 pounds (1,517.466 kilonewtons) of thrust. The rocket was fueled by a highly-refined kerosene, RP-1, with liquid oxygen as the oxidizer.

Friendship 7 is displayed at the Smithsonian National Air and Space Museum.

John Glenn's Mercury spacecraft, Friendship 7, on display at the Smithsonian Institution National Air and Space Museum. (Photo by Eric Long, National Air and Space Museum, Smithsonian Institution.)
John Glenn’s Mercury spacecraft, Friendship 7, on display at the Smithsonian Institution National Air and Space Museum. (Photo by Eric Long, National Air and Space Museum, Smithsonian Institution.)

© 2017, Bryan R. Swopes

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19 February 1986

Mir DOS-7/Proton 8K82K launch at Baikonur Cosmodrome, Site 200, 21:28:23 UTC, 19 February 1986.
Mir DOS-7/Proton 8K82K launch at Baikonur Cosmodrome, Site 200, 21:28:23 UTC, 19 February 1986.

19 February 1986: The core module of the Mir space station (DOS-7) (Dolgovremennaya Orbitalnaya Stanziya) was launched from Site 200 of the Baikonur Cosmodrome aboard a Proton 8K82K rocket. This was the first section of the space station. It consisted of living quarters and environmental systems, engines, and four air locks to which additional modules would be attached.

The Mir was unmanned when it was placed in low Earth orbit. The first two-man crew arrived 15 March 1986 and began bringing the space station systems online. The first expedition stayed aboard for 51 days.

The Mir Core Module was 13.13 meters (43.077 feet) long with a diameter of 4.15 meters (13.616 feet). The solar arrays had a span of 20.73 meters (68.012 feet). The habitable volume of the module was 90 cubic meters (3,178 cubic feet). At launch  it had a mass of 20,400 kilograms (44,974.3 pounds).

The Proton 8K82K was a four-stage liquid-fueled heavy lift rocket. The first stage, Proton K-1, was 21.20 meters (69.554 feet) long with a diameter of 4.15 meters (13.616 feet). Fully fueled, it had a mass of 450,510 kilograms (993,205 pounds). It carried enough hypergolic fuel to power the six RD-253 engines for 124 seconds, producing 67,821.2 kiloNewtons (15,246,812 pounds) of thrust. The second stage, Proton K-2, was 14.00 meters (45.932 feet) long, with the same diameter as the first stage. Its fully-fueled mass was 167,828 kilograms (369,997 pounds). Its four RD-0210 engines burned for 206 seconds, producing 9,596.8 kiloNewtons (2,157,447 pounds) of thrust. The Proton K-3 stage was 6.50 meters (21.326 feet) long, and again, had a diameter of 4.15 meters. The gross mass of the third stage was 50,747 kilograms (111,878 pounds). The single RD-0212 engine burned for 238 seconds, producing 630.2 kiloNewtons (141,675 pounds) of thrust. The final, fourth stage, Proton 11S824, was 5.50 meters (18.045 feet) long with a diameter of 3.70 meters (12.139 feet). Gross mass was 13,360 kilograms (29,454 pounds). It had a single RD-58M engine which burned liquid oxygen and kerosene. It produced 85.02 kiloNewtons (19,113 pounds) of thrust for 610 seconds.

The Proton 8K82K could place a 20,000 kilogram (44,092 pound) payload into low Earth orbit. The rocket was first launched in 1965 and was used until 2003. More than 300 of them were launched.

The Mir space station was continually expanded. It was occupied for 4,592 consecutive days. It remained in orbit until 23 March 2001.

The Mir space station core module (DOS-7) in Earth orbit with solar panel array extended.
The Mir space station core module (DOS-7) in Earth orbit with solar panel array extended.

© 2016, Bryan R. Swopes

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8 February 1973, 02:33:12 UTC

Skylab in Earth orbit, as seen by the departing Skylab 4 mission crew, 8 February 1974. (NASA)
Skylab in Earth orbit, as seen by the departing Skylab 4 mission crew, 8 February 1974. (NASA)

8 February 1973: At 02:33:12 UTC, the Skylab 4/Apollo command module undocked from the Skylab space station in Earth orbit, after 83 days, 4 hours, 38 minutes, 12 seconds. After several orbits, the Apollo capsule reentered the atmosphere and landed in the Pacific Ocean southwest of San Diego California, at 15:16:53 UTC. The crew was recovered by USS Okinawa (LPH-3), a helicopter carrier. Today, the Apollo capsule is displayed at the Smithsonian Institution National Air and Space Museum.

Skylab was an orbital laboratory built from a Saturn S-IVB third stage. It was launched from Cape Canaveral 14 May 1973 as part of a modified Saturn V rocket. The Skylab 4 crew was the third and final group of astronauts to live and the space station. Skylab’s orbit gradually decayed and it re-entered the atmosphere near Perth, Australia, 11 July 1979.

The Skylab 4 mission crew, left to right, Mission Commander Gerald P. Carr, Mission Scientist Edward G. Gibson and Pilot William R. Pogue. Pogue and Carr had joined NASA during the Apollo Program and were scheduled for Apollo 19, which was cancelled. This was the only space flight for these three astronauts. (NASA)
The Skylab 4 mission crew, left to right, Mission Commander Gerald P. Carr, Mission Scientist Edward G. Gibson and Pilot William R. Pogue. Pogue and Carr had joined NASA during the Apollo Program and were scheduled for Apollo 19, which was cancelled. This was the only space flight for these three astronauts. (NASA)

© 2016, Bryan R. Swopes

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7 February 1984

Bruce McCandless outside Challenger in an MMU. (NASA)
Bruce McCandless outside Challenger in a MMU. (NASA)

7 February 1984: During mission STS-41-B, NASA astronauts Captain Bruce McCandless II, United States Navy, and Colonel Robert L. Stewart, United States Air Force, left the Space Shuttle Challenger (OV-099) on the first untethered space walk.

McCandless tested each of the Manned Maneuverung Units (MMU) while Stewart tested a work station. For 5 hours, 55 minutes, they used the nitrogen-fueled Manned Maneuvering Units (MMU) to move about the outside of the space ship. At the farthest, McCandless was 320 feet (98 meters) away from Challenger.

Manned Maneuvering Unit #3 in the collection of the National Air and Space Museum.

The Manned Maneuvering Unit was designed and built by Martin Marietta Corporation (now, Lockheed Martin). It is constructed primarily of aluminum. The MMU is powered by two batteries with 852 watts at full charge, and propelled by 24 gaseous nitrogen thrusters, providing 1.4 pounds of thrust (6.2 newtons), each. The astronaut controls the MMU with two hand controllers. It has six-axis motion and automatic attitude hold. Including a full supply of nitrogen, the MMU weighs approximately 338 pounds (153.3 kilograms). It is designed for a maximum of 6 hours of operation. The unit is 50.0 inches (127.0 centimeters) high, 33.3 inches (84.6 centimeters) wide and with control arms extended, has a maximum depth of 48.0 inches (121.9 centimeters).

Bruce McCandless II (NASA)

Bruce McCandless II is the son of Rear Admiral Bruce McCandless, who was awarded the Medal of Honor for his actions aboard USS San Francisco (CA-38) at the Naval Battle of Guadalcanal, 12–13 November 1942, and grandson of Commodore Byron McCandless. He graduated second in his class at the United States Naval Academy, Annapolis, Maryland, in June 1958 and was trained as a Naval Aviator at Pensacola, Florida. McCandless then served as a fighter pilot, flying the Douglas F-6A Skyray and McDonnell F-4B Phantom II.

Bruce McCandless II was accepted into the NASA astronaut program in 1966. Though he was involved in the Apollo Program, he did not fly until the space shuttle became operational. He served as a Mission Specialist aboard Challenger (STS-41-B) in 1984, and Discovery (STS-31) in 1990.

Captain McCandless has logged over 5,200 hours of flight, and 312 hours, 31 minutes, 1 second in space and completed 208 orbits of the Earth.

Bruce McCandless at a distance of approximately 320 feet (98 meters) from the space shuttle Challenger, 7 February 1984. (NASA)
Captain Bruce McCandless II, U.S. Navy, at a distance of approximately 320 feet (98 meters) from the space shuttle Challenger, 7 February 1984. (NASA)

© 2017, Bryan R. Swopes

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6 February 1971

Alan B. Shepard conducting geological investigation at the Fra Mauro Highlands, 6 February 1971. (NASA)
Alan B. Shepard conducting geological investigation at the Fra Mauro Highlands, 6 February 1971. (Edgar D. Mitchell/NASA)

6 February 1971: During the second EVA of Apollo 14’s mission to The Moon, Mission Commander Alan Bartlett Shepard, Jr., and Lunar Module Pilot Edgar Dean Mitchell conduct a geological exploration of the area near the Antares Lunar Module landing site.

Captain Alan B. Shepard, Jr., USN, during geology training for the upcoming Apollo 14 mission, Arizona, 1970. (NASA)
Captain Alan B. Shepard, Jr., USN, during geology training for the upcoming Apollo 14 mission, Arizona, 1970. (NASA) 

FAI Record File Num #10301 [Direct Link]
Status: ratified – superseded since approved
Region: World
Class: Astronau (Space records)
Sub-Class: K_Absolute (Absolute record for Astronautics)
Category: General
Group: Not applicable
Type of record: Extravehicular duration in space
Performance: 9 hr 12 min 27 sec
Date: 1971-02-09
Course/Location: Cape Kennedy, FL (USA)
Claimant Alan B. Shepard, Jr (USA)
Crew Stuart A. ROOSA, Edgar D. MITCHELL (USA)
Spacecraft: Apollo 14

FAI Record File Num #10304 [Direct Link]
Status: ratified – superseded since approved
Region: World
Class: K (Space records)
Sub-Class: K-3 (Missions to celestial bodies)
Category: Spacecraft with more than one astronaut
Group: General category
Type of record: Extravehicular duration on the surface of the celestial body by an astronaut
Performance: 9 hr 12 min 27 sec
Date: 1971-02-09
Course/Location: Cape Kennedy, FL (USA)
Claimant Alan B. Shepard, Jr (USA)
Crew Stuart A. ROOSA, Edgar D. MITCHELL (USA)
Spacecraft: Apollo 14

FAI Record File Num #10308 [Direct Link]
Status: ratified – superseded since approved
Region: World
Class: K (Space records)
Sub-Class: K-3 (Missions to celestial bodies)
Category: Spacecraft with more than one astronaut
Group: General category
Type of record: Distance covered on foot on the surface of the celestial body
Performance: 1 454 meters
Date: 1971-02-09
Course/Location: Cape Kennedy, FL (USA)
Claimant Alan B. Shepard, Jr (USA)
Crew Edgar D. MITCHELL (USA)
Spacecraft: Apollo 14

FAI Record File Num #10309 [Direct Link]
Status: ratified – superseded since approved
Region: World
Class: K (Space records)
Sub-Class: K-3 (Missions to celestial bodies)
Category: Spacecraft with more than one astronaut
Group: General category
Type of record: Total extravehicular duration on the surface of the celestial body by all crew members
Performance: 17h 33mn 29 sec
Date: 1971-02-09
Course/Location: Cape Kennedy, FL (USA)
Claimant Alan B. Shepard, Jr (USA)
Crew Edgar D. MITCHELL (USA)
Spacecraft: Apollo 14

Astronaut Edgar D. Mitchell, lunar module pilot, photographed this sweeping view showing fellow Moon-explorer astronaut Alan B. Shepard Jr., mission commander, and the Apollo 14 Lunar Module (LM). A small cluster of rocks and a few prints made by the lunar overshoes of Mitchell are in the foreground. Mitchell was standing in the boulder field, located just north by northwest of the LM, when he took this picture during the second Apollo 14 extravehicular activity (EVA-2), on February 6, 1971. (Edgar D. Mitchell/NASA)
Astronaut Edgar D. Mitchell, lunar module pilot, photographed this sweeping view showing fellow Moon-explorer astronaut Alan B. Shepard Jr., mission commander, and the Apollo 14 Lunar Module (LM). A small cluster of rocks and a few prints made by the lunar overshoes of Mitchell are in the foreground. Mitchell was standing in the boulder field, located just north by northwest of the LM, when he took this picture during the second Apollo 14 extravehicular activity (EVA-2), on February 6, 1971. (Edgar D. Mitchell/NASA)

© 2017, Bryan R. Swopes

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