Transtage
Sign in to saveAlso known as Titan Transtage, SSB-10A
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.
Key facts
- Rocket stage.image
- Transtage_rocket_stage.jpg
- Rocket stage.caption
- A Transtage
- Rocket stage.country origin
- United States
- Rocket stage.manufacturer
- Martin Marietta
- Rocket stage.rockets
- Titan III
- Rocket/stage.name
- Engine details
- Rocket/stage.engines
- 2 AJ10-138
- Rocket/stage.thrust
- each
- Rocket/stage.fuel
- Aerozine 50 /
- Rocket/stage.burntime
- 440 seconds
via Wikipedia infobox
Wikidata facts
- Subclass of
- space tug
- Country of origin
- United States
- Diameter
- 3.05
- Mass
- 1950
- Manufacturer
- Martin Marietta
- Image
- Transtage rocket stage.jpg
- Height
- 4.57
Show 2 more facts
- first flight
- 1968-00-00
- Commons category
- Transtage
via Wikidata · CC0
~1 min read
Encyclopedic overview
3 sectionsContents
- History
- See also
- References
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== thumb|Artist's conception of a Titan III Transtage burn 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. 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 of thrust. The design specification required up to three restarts during the first six hours of a mission.
Excerpted from Wikipedia’s “Transtage” article, available under the CC BY-SA 4.0 licence.