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Thrust vector control requirements for launch vehicles using a 260-inch solid rocket first stage
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1969 |
| Description | Gimbaled nozzle and liquid injection thrust vector control requirements for solid rocket two stage launch vehicles |
| File Size | 10688970 |
| Page Count | 59 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19700003019 |
| Archival Resource Key | ark:/13960/t04z01t58 |
| Language | English |
| Publisher Date | 1969-12-01 |
| Access Restriction | Open |
| Subject Keyword | Space Vehicles 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 |