From Wikipedia, the free encyclopedia
Transtage
A Transtage
Manufacturer Martin Marietta
Country of originUnited States
Used on Titan III
General characteristics
Height4.57 meters (15.0 ft)
Diameter3.05 meters (10.0 ft)
Gross mass12,247 kilograms (27,000 lb)
Engine details
Powered by2 AJ10-138
Maximum thrust8,000 lbf (36 kN) each [1]
Specific impulse311 seconds (3.05 km/s)
Burn time440 seconds
Propellant Aerozine 50 / N2O4

Transtage, given the United States Air Force designation SSB-10A, was an American upper stage used on Titan III rockets, developed by Martin Marietta and Aerojet.

History

Transtage was developed in anticipation of a requirement to launch military payloads to geostationary orbit; a contract for development of the stage was issued on 20 August 1962. [2] Transtage used a pressure-fed two-chamber configuration, using Aerozine 50 fuel and nitrogen tetroxide as oxidizer; the thrust chambers were gimbaled for steering and each produced 8,000 lbf (36 kN) of thrust. The design specification required up to three restarts during the first six hours of a mission. [3]

Forty-seven Titan III launches are known to have used Transtage upper stages; of those, three are known to have suffered launch failures. [4] The first launch, boosted by a Titan IIIA, occurred on 1 September 1964; the Transtage failed to pressurize, resulting in premature engine cutoff, and a failure to reach orbit. [4] The second launch, on 10 December, was successful, and all ensuing launches used the Titan IIIC launch vehicle. The last launch of a Transtage was on 4 September 1989, boosted by a Titan 34D rocket. [4]

See also

References

Citations

  1. ^ Wade, Mark. "AJ10-138". Encyclopedia Astronautica. Archived from the original on December 28, 2016. Retrieved 2019-07-24.
  2. ^ Foradori, Giacomoello and Pascolini 2017, pp.56-57
  3. ^ Hunley 2007, p. 168.
  4. ^ a b c Heyman 2003

Bibliography

  • Foradori, Paolo; Giampiero Giacomello; Alessandro Pascolini (2017). Arms Control and Disarmament: 50 Years of Experience in Nuclear Education. London: Palgrage Macmillan. ISBN  978-3-319-62258-3.
  • Heyman, Jos (17 March 2003). "Martin Marietta SSB-10 Transtage". Directory of U.S. Military Rockets and Missilesm Appendix 3: Space Vehicles. Designation-Systems. Retrieved 2017-12-17.
  • Hunley, J.D. (2007). The Development of Propulsion Technology for U.S. Space-Launch Vehicles, 1926-1991. College Station, TX: Texas A&M University Press. ISBN  978-1-58544-588-2.

External links