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Wind-tunnel investigation of Saturn S-IC AERODYNAMIC engine gimbal forces and base pressures using a cold-flow-jet simulation technique
- Publication Year :
- 1967
- Publisher :
- United States: NASA Center for Aerospace Information (CASI), 1967.
-
Abstract
- Aerodynamic hinge moments for scale model boost stage nozzle of Saturn V launch vehicle during cold flow jet simulation
- Subjects :
- Space Vehicles
Subjects
Details
- Language :
- English
- Database :
- NASA Technical Reports
- Notes :
- 128-31-11-03-22
- Publication Type :
- Report
- Accession number :
- edsnas.19670030895
- Document Type :
- Report