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Titan IIIA

Spacecraft and Launch Vehicles

The Titan IIIA was an American expendable launch vehicle in the Titan rocket family, flown only four times in 1964 and 1965 as a test bed for the Transtage upper stage that was meant for the larger Titan IIIC. It stacked the Transtage on top of two core stages derived from the Titan II missile, and the same core later served as the center of the Titan IIIC. Its first flight, on 1 September 1964, ended short of orbit because the Transtage failed to pressurize and shut down early. A second test on 10 December 1964 succeeded, and two more launches in 1965 carried Lincoln Experimental Satellites before the vehicle was retired. It was built in the lineage of the Martin company, later Martin Marietta, whose Titan program it belonged to, and it is the prototype step between the Titan II and the heavier Titan III variants that followed.

Facts
Year
1964 1
Propulsion
Aerozine 50 and nitrogen tetroxide 2
Status
Retired from service 1
Comparison
Body Style
Launch vehicle 1
Connections

Exemplifies

Source Titan IIIA (Wikipedia)
In the Other Atlases

Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source Encyclopedia Astronautica: Titan (Encyclopedia Astronautica)Titan III program history
Quote, Titan III program history
Martin Marietta Corporation would be the systems integration (prime) contractor for the Titan III program that was managed by AFSC's Space Systems Division.

Originated In

Also in Geography Atlas: where this subject originated.

Source Titan IIIA (Wikipedia)Lead
Quote, Lead
The Titan IIIA or Titan 3A was an American expendable launch system
Sources
1. Titan IIIA (Wikipedia)
  • Lead, first flight
    the Titan IIIA made its first flight on 1 September 1964
  • Lead
    The Titan IIIA or Titan 3A was an American expendable launch system
  • Lead, retirement
    before the Titan IIIA was retired
View the Source
2. Encyclopedia Astronautica: Titan IIIA (Encyclopedia Astronautica)
Encyclopedia AstronauticaStage data
Quote, Stage data
Propellants: N2O4/Aerozine-50.
View the Source
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