Systems aspects of the lunar survey viewfinder /LSV/.
Aerodynamic Characteristics of 0.187-Scale Model of a Target Missile at Mach 1.80 to 2.16
Acquisition of APOLLO Using the 12 Ft Entry Ship U S B-System
Passive infrared acquisition and tracking system analysis, task II
In a Difficult Aerial Situation (V Slozhnoe Obstanovke)
Study Plan for an Investigation of Target Acquisition With a Radar-Aided Electro-Optical Missile
Hybrid Propulsion System for an Advanced Rocket-Powered Target Missile
Hybrid Propulsion System for an Advanced Rocket-Powered Target Missile
Hypervelocity Impact Damage in Aluminum Targets Final Report