Contents: Stability and Control - Volume 1 (18 Jan '68), Volume 2 (8 Mar '68); Stress Analysis (Structural analysis of 2.75 inch diameter rocket motor - Feb '68, Rev. May '68); Weights and Balance; Environmental Test.
2.75-In. Folding Fin Aircraft Rocket. Volume 2. Appendixes
1969
360 pages
Report
No indication
English
Rockets , Rocket Engines & Motors , Solid propellant rocket engines , Aircraft ammunition , Folding fins(Rockets) , Stability , Performance(Engineering) , Stresses , Deformation , Weight , Load distribution , Aerodynamic characteristics , Aeroelasticity , Aerodynamic heating , Wind tunnel models , Model tests , Structures , Solid rocket propellants , Mathematical models , Exterior ballistics , Visual inspection , Vibration , Altitude , Temperature , Humidity , X ray photography , Rocket propellant grains , Shock resistance , Environmental tests , Folding fin aircraft rockets , Ffar(Folding fin aircraft rockets) , 2.75-in. rockets
2.75-In. Folding Fin Aircraft Rocket. Volume 1
NTIS | 1969
|Service Test of XM200 2.75-Inch Aircraft Rocket Launcher
NTIS | 1969
|An improved Canadian 2.75-inch rocket motor
AIAA | 1976
An Improved Canadian 2.75-Inch Rocket Motor
NTIS | 1976
|