Centaur capabilities for communications satellite launches
Abstract
The configurations, payload capabilities, and payload envelopes for Centaur in various applications are presented. The Centaur launch record is summarized and the Atlas/Centaur launch schedule is shown. Improvements in capability are reported on, and current and proposed vehicles are depicted. Dual Delta class spacecraft will be flown using a tandem adapter or large direct broadcast satellites in a single launch model. Shuttle/Centaur will permit spacecraft weights of up to 14,000 lb to be put into orbit, including payload lengths up to 40 ft. A new capability to transfer large deployed space systems from the Shuttle to high-altitude orbits at low thrusts will be available. Spacecraft lengths requiring the full, 60-foot cargo bay and weighing 20,000 lb could be placed in geosynchronous orbit with on-orbit rendezvous and assembly of the Centaur and spacecraft in low earth orbit.
- Publication:
-
9th Communications Satellite Systems Conference
- Pub Date:
- March 1982
- Bibcode:
- 1982coss.conf.....R
- Keywords:
-
- Atlas Centaur Launch Vehicle;
- Communication Satellites;
- Geosynchronous Orbits;
- Orbital Assembly;
- Spacecraft Launching;
- Transfer Orbits;
- High Altitude;
- Low Thrust Propulsion;
- Payloads;
- Space Rendezvous;
- Titan Centaur Launch Vehicle;
- Launch Vehicles and Space Vehicles