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Geostationary earth science platform concepts
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Herardian, M. M. |
| Copyright Year | 1989 |
| Description | The new concepts are presented for the Geostationary Earth Science Platform. Bus and payload arrangements, with instrument locations on the payload module and basic payload dimensions, are depicted and compared for each concept. The Titan 4 SRMU (with solid rocket motor upgrage) launch vehicle is described and compared to the standard Titan 4. The upgraded Titan 4 is capable of launching a 13,500 lb payload to GEO. The launch configuration showing each concept packaged within the 16 ft diameter payload envelope is presented. This presentation is represented by viewgraph only. |
| File Size | 552755 |
| Page Count | 8 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19900009936 |
| Archival Resource Key | ark:/13960/t6b32rw8z |
| Language | English |
| Publisher Date | 1989-07-01 |
| Access Restriction | Open |
| Subject Keyword | Spacecraft Design, Testing And Performance Position Location Solid Propellant Rocket Engines Earth Sciences Titan Launch Vehicles Geosynchronous Orbits Spacecraft Launching Synchronous Platforms Payloads Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
