The report presents the results of a parametric study conducted to determine the general physical and performance characteristics of a group of all-weather, air defense missiles capable of engaging low-flying threat aircraft to the Field Army in the 1975-1980 time frame. Preliminary missile designs are presented which meet the study objectives, and the advantages of a boost-sustain motor over an all-boost design are discussed. (Author)
Parametric Missile Design Study for an All-Weather, Low Altitude Air Defense System (AWLAADS)
1972
186 pages
Report
No indication
English
Surface Launched Missiles , Antiaircraft Defense Systems , Antiaircraft defense systems , Surface to air missiles , Configuration , Solid propellant rocket motors , Experimental design , Line of sight , Performance(Engineering) , Low altitude , AWLAADS(All Weather Low Altitude Air Defense Systems) , All weather low altitude air defense systems
Missile guidance for low altitude air defense
AIAA | 1978
|Missile guidance for low altitude air defense
Tema Archive | 1978
|