Loading...
Please wait, while we are loading the content...
Similar Documents
Mars geoscience orbiter and lunar geoscience orbiter
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Fuldner, W. V. Kaskiewicz, P. F. |
| Copyright Year | 1983 |
| Description | The feasibility of using the AE/DE Earth orbiting spacecraft design for the LGO and/or MGO missions was determined. Configurations were developed and subsystems analysis was carried out to optimize the suitability of the spacecraft to the missions. The primary conclusion is that the basic AE/DE spacecraft can readily be applied to the LGO mission with relatively minor, low risk modifications. The MGO mission poses a somewhat more complex problem, primarily due to the overall maneuvering hydrazine budget and power requirements of the sensors and their desired duty cycle. These considerations dictate a modification (scaling up) of the structure to support mission requirements. |
| File Size | 15208043 |
| Page Count | 237 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19830014009 |
| Archival Resource Key | ark:/13960/t06x4614b |
| Language | English |
| Publisher Date | 1983-01-28 |
| Access Restriction | Open |
| Subject Keyword | Launch Vehicles And Space Vehicles Mars Probes Attitude Inclination Explorer Satellites Dynamics Explorer Satellites Lunar Orbiter Spacecraft Design Propulsion System Configurations Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |