Study of the optimization of satellite system design for transfer orbit
Abstract
Geostationary transfer orbit (GTO) characteristics of former geosynchronous satellites; satellite configurations as to GTO requirements; telemetry and telecommand, thermal, power, and attitude control subsystems as to stabilization modes and GTO constraints; and apogee injection strategies (single/multiple burn, steering law) were reviewed. The investigations were confined to 2 Ariane 4 payload classes (2500 kg in GTO, dual-launch and 4200 kg in GTO, single launch), three-axis or slow barbecue stabilization during transfer orbit, and use of a liquid apogee injection system with low thrust level (400 N). A recommendation for an overall system optimization is presented.
- Publication:
-
Final Report Messerschmitt-Boelkow-Blohm G.m.b.H
- Pub Date:
- April 1983
- Bibcode:
- 1983mbbg.reptR....B
- Keywords:
-
- Geosynchronous Orbits;
- Orbital Mechanics;
- Satellite Design;
- Systems Analysis;
- Transfer Orbits;
- Apogees;
- Launch Windows;
- Satellite Configurations;
- Satellite Control;
- Astrodynamics