The new Centaur
Abstract
Two versions of a modified Centaur upper stage, to be carried aboard Shuttles Challenger and Atlantis, are being developed. The G type version, to be used by the Air Force, will provide greater space for larger satellites weighing up to 4800 kg. The G-prime version, to be used by NASA for the first time for the launches of Galileo and the International Solar Polar Mission in 1986, will be a higher performance rocket stage capable of transferring a 6350 kg payload to geostationary orbit. Centaur signals would be relayed through the TDRS satellites by an S-band transmitter, and a dump system would jettison all of the propellant before the stage would be released in the event of a launch abort, or a failure. With the Shuttle, the Centaur G family may provide a flexibility never before available on earlier missions: the carrying of larger cargoes to geostationary orbit, the ability to carry dual payloads, and docking and low thrust transfers.
- Publication:
-
Spaceflight
- Pub Date:
- October 1984
- Bibcode:
- 1984SpFl...26..358P
- Keywords:
-
- Centaur Launch Vehicle;
- Inertial Upper Stage;
- Performance Prediction;
- Solid Propellant Rocket Engines;
- Atlas Centaur Launch Vehicle;
- Challenger (Orbiter);
- Space Shuttle Payloads;
- Technological Forecasting;
- Launch Vehicles and Space Vehicles