The two-stage Advanced Terrier (BT-3)-Sandhawk is a solid propellant, unguided rocket system capable of carrying a 200-pound payload to 1,400,000 feet. A 13-inch diameter ogive-cylinder has sufficient volume for a variety of rocket launched experiments. This report includes aerodynamic, performance, and flight test data, together with the results of wind effect and dispersion analyses. (Author)
Aeroballistic, Performance, Wind Effects, and Impact Dispersion Analyses, and Flight Test Data for the Two-Stage Terrier (Bt-3)-Sandhawk Rocket System
1969
166 pages
Report
Keine Angabe
Englisch
Rockets , Missile Trajectories & Reentry Dynamics , Detonations, Explosion Effects, & Ballistics , Sounding rockets , Aerodynamic characteristics , Rocket motors(Solid propellant) , Rocket trajectories , Payload , Flight testing , Aerodynamic loading , Stability , Impact prediction , Fins , Exterior ballistics , Terrier , Sandhawk sounding rockets , BT-3 rockets , Six degrees of freedom