Manned Orbiting Laboratory

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Manned Orbiting Laboratory
Gemini reentry capsule separates from the orbiting MOL
A 1967 conceptual drawing of the Gemini B reentry capsule separating from the MOL at the end of a mission
Station statistics
Crew 2
Mission status Cancelled
Mass 31,910 lb (14,470 kg)
Length 71.9 ft (21.9 m)
Diameter 10.0 ft (3.0 m)
Pressurised volume 400 cu ft (11.3 m3)
Orbital inclination polar or sun synchronous orbit
Days in orbit 40 days
Configuration
Vertical model showing sections of the MOL and Gemini B capsule
Configuration of the Manned Orbital Laboratory

The Manned Orbiting Laboratory (MOL), originally referred to as the Manned Orbital Laboratory, was part of the United States Air Force's manned spaceflight program, a successor to the cancelled Boeing X-20 Dyna-Soar military reconnaissance space plane project. The project was developed from several early Air Force and NASA concepts of manned space stations to be used for reconnaissance purposes. MOL evolved into a single-use laboratory, with which crews would be launched on 40-day missions and return to Earth using a Gemini B spacecraft, derived from NASA's Gemini program.

The MOL program was announced to the public on 10 December 1963 as a manned platform to prove the utility of man in space for military missions. Astronauts selected for the program were later told of the reconnaissance mission for the program.[1] The contractor for the MOL was the Douglas Aircraft Company. The Gemini B was externally similar to NASA's Gemini spacecraft, although it underwent several modifications, including the addition of a circular hatch through the heat shield, which allowed passage between the spacecraft and the laboratory.[2]

MOL was cancelled in 1969, during the height of the Apollo program, when it was shown that unmanned reconnaissance satellites could achieve the same objectives much more cost-effectively. U.S. space station development was instead pursued with the civilian NASA Skylab (Apollo Applications Program) which flew in the mid-1970s.

In the 1970s, the Soviet Union launched three Almaz military space stations, similar in intent to the MOL, but cancelled the program in 1977 for the same reasons.

History[edit]

See also: OPS 0855

There was one test flight of an MOL mockup that was built from a Titan II propellant tank. The Gemini 2 spacecraft was re-flown on a 33-minute sub-orbital test flight. After the Gemini was separated for its sub-orbital reentry, the MOL mockup continued on into orbit and released three satellites. A hatch was installed in the Gemini 2 heat shield to provide access to the MOL and was tested in the sub-orbital reentry. The test flight was launched by the USAF on 3 November 1966 at 13:50:42 UTC on launch vehicle Titan IIIC-9 from LC-40 at Cape Canaveral Air Force Station. The Gemini 2-MOL space capsule was recovered near Ascension Island in the South Atlantic by the USS La Salle.

The MOL was planned to use a helium-oxygen atmosphere. It used a Gemini B spacecraft as a reentry vehicle. The crew were to be launched with the Gemini B and MOL, and returned to Earth in the Gemini B. They would conduct up to 40 days of military reconnaissance using large optics, cameras, and side-looking radar.

The USAF Astronaut Maneuvering Unit (AMU) was developed for the MOL project. NASA chief astronaut Deke Slayton later speculated in his autobiography that the AMU may have been developed for MOL because the Air Force "thought they might have the chance to inspect somebody else's satellites."[3]

In response to the announcement of the MOL, the USSR commissioned the development of its own military space station, Almaz. Three Almaz space stations flew as Salyut space stations, and the program also developed a military add-on used on Salyut 6 and Salyut 7.[4][5][6]

In 2005, two MH-7 training space suits from the MOL program were discovered in a locked room in the Launch Complex 5/6 museum on Cape Canaveral.[7]

MOL astronauts[edit]

14 of the 17 MOL astronauts:
Top row L-R: Herres, Hartsfield, Overmyer, Fullerton, Crippen, Peterson, Bobko, Abrahamson.
Bottom Row L-R: Finley, Lawyer, Taylor, Crews, Neubeck, Truly.
  • MOL Group 2 - June 1966
    • Karol J. Bobko USAF — Pilot, STS-6, Commander, STS-51-D. STS-51-J
    • Robert L. Crippen USN — Pilot, STS-1, Commander, STS-7, STS-41C, STS-41G; Director, Kennedy Space Center, 1992–95
    • C. Gordon Fullerton USAF (1936-2013) — Pilot, Space Shuttle Enterprise ALT #1, STS-3, Commander, STS-51-F
    • Henry W. Hartsfield, Jr. USAF — Pilot, STS-4, Commander, STS-41-D, STS-61-A; Director, Human Exploration and Development of Space Independent Assurance
    • Robert F. Overmyer USMC (1936-1996) — Pilot, STS-5, Commander: STS-51-B; killed in Cirrus crash, 22 March 1996
MOL test launch OPS 0855, 3 November 1966, Cape Canaveral, Fla.

MOL flight schedule[edit]

Completed[edit]

  • 1966 November 3 - MOL mockup - refurbished Gemini 2 capsule launched unmanned

Proposed[edit]

  • 1970 December 1 - MOL 1 - First unmanned Gemini-B/Titan 3M qualification flight (Gemini-B flown alone, without an active MOL).
  • 1971 June 1 - MOL 2 - Second unmanned Gemini-B/Titan 3M qualification flight (Gemini-B flown alone, without an active MOL).
  • 1972 February 1 - MOL 3 - A crew of two (James M. Taylor, Albert H. Crews) would have spent thirty days in orbit.
  • 1972 November 1 - MOL 4 - Second manned mission.
  • 1973 August 1 - MOL 5 - Third manned mission.
  • 1974 May 1 - MOL 6 - Fourth manned MOL mission. All Navy crew composed of Richard H. Truly and Robert Crippen.
  • 1975 February 1 - MOL 7 - Fifth manned MOL.

Operational MOLs were to be launched on Titan IIIM rockets from SLC-6 at Vandenberg AFB, California and LC-40 at Cape Canaveral Air Force Station, Florida.[citation needed]

KH-10[edit]

Main article: KH-10 Dorian
KH-10 mission module

Starting in 1965 a large optical system was added to the spacecraft for military reconnaissance. This camera system was codenamed Dorian and given the designation KH-10. The project was canceled on 10 June 1969 before any operational flights occurred.

The KH-10 intended for the MOL program was succeeded by the unmanned KH-11 Kennan, which launched in 1976 as the Soviet Union was winding down its manned space reconnaissance program. The KH-11 achieved the goal of 3-inch (76 mm) imaging resolution and introduced video transmission of images back to Earth.[1]

Cancellation[edit]

The program was canceled on 10 June 1969 with the first projected flight three years away. Between 1965 and 1969, MOL's projected cost rose from $1.5 billion to $3 billion while the Vietnam War took larger portions of the defense budget. While Defense Secretary Melvin R. Laird and the Joint Chiefs of Staff strongly supported the station, Central Intelligence Agency head Richard Helms did not support the project because he feared that the death of a MOL astronaut might ground launches and thus damage the nation's satellite reconnaissance program. President Richard Nixon and National Security Advisor Henry Kissinger agreed to the Bureau of the Budget's proposal to cancel MOL,[8] as it was determined the capabilities of unmanned spy satellites met or exceeded the capabilities of manned MOL missions.

NASA offered those under 35 years of age the opportunity to transfer to its astronaut program. Seven of the 14 MOL astronauts were younger than 35 and took the offer, becoming NASA Astronaut Group 7: future NASA Administrator Richard H. Truly, Karol J. Bobko, Robert Crippen, C. Gordon Fullerton, Henry W. Hartsfield, Robert F. Overmyer, and Donald H. Peterson. All flew on the Space Shuttle.

The Gemini 2 capsule used in the only flight of the MOL program is on display at the Air Force Space & Missile Museum at Cape Canaveral Air Force Station.[9] A test article at the National Museum of the United States Air Force, Wright-Patterson AFB, Ohio, is the Gemini B spacecraft (sometimes confused with Blue Gemini). It is recognized by its distinctive "US Air Force" written on the side, and the circular hatch cut through the heat shield.[10]

Specifications[edit]

MOL main features
  • Crew: 2
  • Maximum duration: 40 days
  • Orbit: Sun synchronous or polar
  • Length: 71.9 ft (21.92 m)
  • Diameter: 10.0 ft (3.05 m)
  • Cabin Volume: 400 cu ft (11.3 m3)
  • Mass: 31,914 lb (14,476 kg)
  • Payload: 6,000 lb (2,700 kg)
  • Power: fuel cells or solar cells
  • RCS system: N2O4/MMH

Gallery[edit]

See also[edit]

References[edit]

  1. ^ a b "NOVA: Astrospies". PBS. Retrieved 13 October 2011. 
  2. ^ Slayton & Cassutt 1994, p. 249.
  3. ^ Slayton & Cassutt 1994, p. 174.
  4. ^ "The Almaz program". Russian Space Web. Retrieved 12 February 2011. 
  5. ^ Wade, Mark. "Almaz". Encyclopedia Astronautica. Retrieved 12 February 2011. 
  6. ^ Grahn, Sven. "The Almaz Space Station Program". Sven's Space Place. Retrieved 12 February 2011. 
  7. ^ Nutter, Ashley (2 June 2005). "Suits for Space Spies". NASA.gov. Retrieved 12 February 2011. 
  8. ^ Heppenheimer, T. A. (1998). The Space Shuttle Decision. NASA. pp. 204–205. OCLC 40305626. SP-4221. 
  9. ^ "Gemini Capsule". Air Force Space & Missile Museum. Retrieved 17 June 2014. 
  10. ^ "Gemini Spacecraft". National Museum of the US Air Force. 7 March 2007. Retrieved 12 February 2011. 

Bibliography[edit]

External links[edit]