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Aerospace vehicle
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Jackson, L. R. |
| Copyright Year | 1985 |
| Description | A dual structure aerospace vehicle is described which has an aeroshell structure and an internally disposed separable and reusable integral tank/thrust structure. The tank/thrust structure is inuslated for cryogenic fuels and the cavity within aeroshell is insulated from the tank/thrust structure. An internal support ring within the cavity serves as an attachment for lugs on the tank/thrust structure via double hinges. The aft end of tank/thrust structure is provided with rocket engines and exit nozzles with a trunnion supporting the tank/thrust structure within the aeroshell. |
| File Size | 609556 |
| Page Count | 10 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19860009839 |
| Archival Resource Key | ark:/13960/t47q3vt7x |
| Language | English |
| Publisher Date | 1985-12-10 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Design, Testing And Performance Hinges Insulation Aerospace Vehicles Airframes Spacecraft Components Reusable Spacecraft Propellant Tanks Propulsion System Configurations Spacecraft Design Shafts Machine Elements Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Patent |
