Cost reduction for communication satellites in the 1800 to 2600 kg (GEO) class by a standardized propulsion module (OPM)
Abstract
The standardized propulsion module for future spacecraft in the 1800-2700 kg class is described. The definition of the propulsion system and its thrust level are addressed, and the design of the orbital propulsion module (OPM) is shown and described. The masses of various components are given. The OPM application and size optimization for the Ariane 4 launchers are examined, and the cost-saving aspects of OPM and its space applications are discussed.
- Publication:
-
Stockholm International Astronautical Federation Congress
- Pub Date:
- October 1985
- Bibcode:
- 1985stoc.iafcQQ...K
- Keywords:
-
- Communication Satellites;
- Cost Reduction;
- Propulsion System Configurations;
- Spacecraft Propulsion;
- Synchronous Satellites;
- Apogees;
- Ariane Launch Vehicle;
- Cost Effectiveness;
- Gimbals;
- Rocket Thrust;
- Transfer Orbits;
- Launch Vehicles and Space Vehicles