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Liquid rocket booster study. volume 2, book 6, appendix 10: vehicle systems effects
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1989 |
| Description | Three tasks were undertaken by Eagle Engineering as a part of the Liquid Rocket Booster (LRB) study. Task 1 required Eagle to supply current data relative to the Space Shuttle vehicle and systems affected by an LRB substitution. Tables listing data provided are presented. Task 2 was to evaluate and compare shuttle impacts of candidate LRB configuration in concert with overall trades of analysis activity. Three selected configurations with emphasis on flight loads, separation dynamics, and cost comparison are presented. Task 3 required the development of design guidelines and requirements to minimize impacts to the Space Shuttle system from all LRB substitution. Results are presented for progress to date. |
| File Size | 5004904 |
| Page Count | 132 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19900000822 |
| Archival Resource Key | ark:/13960/t1kh5gt4w |
| Language | English |
| Publisher Date | 1989-03-24 |
| Access Restriction | Open |
| Subject Keyword | Spacecraft Propulsion And Power Stage Separation Launch Vehicles Propulsion System Performance Space Shuttles Cost Analysis Liquid Propellant Rocket Engines Booster Rocket Engines Propulsion System Configurations Aerodynamic Loads Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
