Thrust Vector Control Requirements for Solid- Propellant Launch Vehicles
1967
31 pages
Report
Keine Angabe
Englisch
Space Launch Vehicles & Support Equipment , Deflection , Solid propellant rocket engine , Thrust vector control (tvc) , Aerodynamic , Angle , Apollo spacecraft , Canard , Configuration , Control , Density , Fin , Fixed , Launch vehicle , Load , Moving , Propellant , Saturn s- ivb stage , Shroud , Solid , Surface , Thrust , Trajectory , Vector , Voyager project , Wind