MARS OBSERVER MISSION AND SYSTEMS OVERVIEW

被引:3
作者
PALOCZ, S
机构
[1] General Electric Company, Princeton, NJ
[2] Astro-Space Division
关键词
D O I
10.2514/3.26271
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The objective of the Mars Observer mission is the scientific investigation of the planet's surface, atmosphere, and gravitational and magnetic fields. The Mars Observer spacecraft provides a three-axis-stabilized platform for the payload system. This spacecraft is the first in a planned series of planetary orbiters that use Earth-orbiting design heritage adapted to planetary exploration mission objectives. The operation of the payload instruments is based on a new distributed concept, providing home-based commanding capabilities for the science investigators. The spacecraft will be launched during the September/October opportunity of 1992 and will travel approximately 11 months to Mars. During a two-year mapping period, the spacecraft will be placed in a nearly circular, low-altitude, Sun-synchronous orbit with a repeat cycle of 7 Martian days. At the end of the mission, the spacecraft will relay scientific information from scientific equipment, placed on the Martian surface, as part of a joint American, Soviet, and French experiment.
引用
收藏
页码:491 / 497
页数:7
相关论文
共 7 条
[1]  
BEERER JG, 1989, 891961 AM ASTR SOC P
[2]  
BLUME WH, 1990, 6422311 JET PROP LAB
[3]  
ESPOSITO PB, 1989, 2ND AIAA JPL INT C S
[4]  
KOMRO F, 1989, AIAA890258 PAP
[5]  
POTTS DL, 1989, AIAA890255 PAP
[6]  
UPHOFF C, 1984, AIAA840318 PAP
[7]  
1990, TIIIMOTOS00370 MART