The aerodynamic and mechanical design aspects and the performance analysis for the TATER rocket system are discussed. The TATER is a three-stage, solid-propellant rocket system capable of boosting a 70-lb recoverable payload to velocities of 10,500 to 11,000 ft/s in approximately 12 seconds from launch with a maximum velocity altitude variation of 10,000-30,000 ft on an ascent trajectory. (ERA citation 01:011224)
Aeroballistic and Mechanical Design and Development of the Talos-Terrier-Recruit (Tater) Rocket System with Flight Test Results
1976
120 pages
Report
Keine Angabe
Englisch
Rockets , Nose cones , Ablation , Aerodynamics , Design , Performance , Reentry , Test facilities , Testing , ERDA/420200 , TATER launch vehicles
Engineering Index Backfile | 1929