Add to ORKGThe Aerospike drag reduction mechanism was designed and developed for use on the Trident I submarine launched ballistic missile. This mechanism encounters a unique combination of environments necessitating unique design solutions to ensure satisfactory operation over its design life. The development of the Aerospike is reviewed emphasizing the unique and interesting problems encountered and their solutions
Fragment hit density and hit probability of the warhead are the critical parameters in the selectio...
The staging mechanisms of the Japanese satellite launch vehicle Mu-3SII involving a unique separatio...
High subsonic wind tunnel study of stability and control characteristics of antitank missile with ra...
ASALM (Advanced Strategic Air-Launched Missile) is a supersonic air vehicle designed to be air-launc...
Up until recent years, the guidance systems of missiles have been the limiting factor for the range ...
Future Indian Air force and Navy Capabilities indicate the need for a supersonic cruise missile. The...
A series of wind tunnel tests have been performed on an aerospike-protected missile dome at a Mach n...
A Propulsion system is designed and developed for the third generation antitank guided missile (ATG...
A wind-tunnel investigation has been performed at low supersonic speeds (at Mach numbers of 1.60, an...
A high lift-to-drag ratio is considered crucial for high-altitude and long-endurance hypersonic vehi...
This project proposes the demonstration of a novel, compact propulsion system, scaled for CubeSat-si...
The development of missiles from early history up to about 1970 is discussed. Early unpowered missil...
A preliminary investigation was conducted to determine whether a warhead stage of an antimissile mis...
Annular spike nozzle engines have long been the holy grail of rocket engine design, promising superi...
An investigation was made to determine the aerodynamic characteristics of an airbreathing missile co...
Fragment hit density and hit probability of the warhead are the critical parameters in the selectio...
The staging mechanisms of the Japanese satellite launch vehicle Mu-3SII involving a unique separatio...
High subsonic wind tunnel study of stability and control characteristics of antitank missile with ra...
ASALM (Advanced Strategic Air-Launched Missile) is a supersonic air vehicle designed to be air-launc...
Up until recent years, the guidance systems of missiles have been the limiting factor for the range ...
Future Indian Air force and Navy Capabilities indicate the need for a supersonic cruise missile. The...
A series of wind tunnel tests have been performed on an aerospike-protected missile dome at a Mach n...
A Propulsion system is designed and developed for the third generation antitank guided missile (ATG...
A wind-tunnel investigation has been performed at low supersonic speeds (at Mach numbers of 1.60, an...
A high lift-to-drag ratio is considered crucial for high-altitude and long-endurance hypersonic vehi...
This project proposes the demonstration of a novel, compact propulsion system, scaled for CubeSat-si...
The development of missiles from early history up to about 1970 is discussed. Early unpowered missil...
A preliminary investigation was conducted to determine whether a warhead stage of an antimissile mis...
Annular spike nozzle engines have long been the holy grail of rocket engine design, promising superi...
An investigation was made to determine the aerodynamic characteristics of an airbreathing missile co...
Fragment hit density and hit probability of the warhead are the critical parameters in the selectio...
The staging mechanisms of the Japanese satellite launch vehicle Mu-3SII involving a unique separatio...
High subsonic wind tunnel study of stability and control characteristics of antitank missile with ra...