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Feasibility study of litvc for shuttle srb
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Martin, C. L. Powers, L. B. |
| Copyright Year | 1981 |
| Description | A liquid injection thrust vector control (LITVC) system for the shuttle solid rocket booster (SRB) was analyzed. The LITVC was compared with the SRB baseline flexible seal. A table of LITVC advantages and disadvantages is presented. It is concluded that the LITVC performs well at low to moderate duty cycles, but not for high duty cycle requirements. |
| File Size | 565845 |
| Page Count | 28 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19810024688 |
| Archival Resource Key | ark:/13960/t28961844 |
| Language | English |
| Publisher Date | 1981-09-01 |
| Access Restriction | Open |
| Subject Keyword | Spacecraft Propulsion And Power Injectors Launch Vehicles Propulsion System Performance Thrust Vector Control Automatic Flight Control Feasibility Analysis Liquid Injection Booster Rocket Engines Space Shuttle Boosters 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 |
