Wind Tunnel Investigation of Saturn S-IC Aerodynamic Engine Gimbal Forces and Base Pressures Using a Cold-Flow-Jet Simulation Technique
Wind Tunnel Investigation of Saturn S-IC Aerodynamic Engine Gimbal Forces and Base Pressures Using a Cold-Flow-Jet Simulation Technique
United States. National Aeronautics and Space Administration., NASA
Details
- OL Work ID
- OL28575894W