This study was conducted to determine the suspension needs of the LANCE Limited Mobility Launcher. A search of operational launcher test data was conducted and a parametric study of the LANCE concept was made. The results of these studies indicated that the launcher should be equipped with a sprung, damped suspension which will give the towed launcher mobility commensurate with the towing vehicle. (Author)
Studies Performed to Determine Suspension Needs for Lance Limited Mobility Launcher
1963
62 pages
Report
Keine Angabe
Englisch
Missile Launching & Support Systems , Rockets , Guided missile launchers , Suspension devices , Rocket launchers , Failure(Mechanics) , Reduction , Accelerometers , Mobility , Fatigue(Mechanics) , Computer programming , Weight , Towing vehicles , Mathematical models , Damping , Tow bars , Torsion bars , Vibration isolators , Stresses , Costs , Compatibility , Honest john , Lance missiles , Little john
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