This contract covers the design, development, testing and delivery of an improved rocket for the flechette warhead. Work included (1) design, analysis, and component tests; (2) development tests; (3) Preliminary Flight Rating Tests; and (4) delivery of improved rocket motors. Analyses included design trade-off studies, aerodynamics analysis, and manufacturing optimization studies. The improved design was successfully demonstrated through the preliminary flight rating tests and through flight tests, both ground-launched and aircraft-launched. Performance, reliability, and accuracy are within contract requirements. This final report is in two volumes. Volume I contains the program accomplishments and Volume II (AD-501 433) contains the Appendixes. (Author)
2.75-In. Folding Fin Aircraft Rocket. Volume 1
1969
258 pages
Report
No indication
English
Rockets , Rocket Engines & Motors , Detonations, Explosion Effects, & Ballistics , Solid propellant rocket engines , Aircraft ammunition , Folding fins(Rockets) , Rocket propellant grains , Rocket nozzles , Flechettes , Stresses , Rocket warheads , Thermal stresses , Rocket engine cases , Storage , Nozzle closures , Stability , Nozzle inserts , Test methods , Thrust , Manufacturing , Performance(Engineering) , Erosion , Reliability , Configuration , Accuracy , Pressure , Interior ballistics , Exterior ballistics , Misalignment , Fin stabilized ammunition , Mathematical models , Launching , Velocity , Airborne , Flight testing , Rocket igniters , Solid rocket propellants , Ffar(Folding fin aircraft rockets) , Folding fin aircraft rockets , 2.75-in. rockets , Pban propellant ingredient , Tradeoffs
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