This report presents studies to determine an optimum static lunette load for the LANCE lightweight launcher. Included are studies pertaining to prime mover and launcher dynamics, grade ability, braking loads, stopping distance, and human factors of manhandling the launcher. (Author)
Studies to Determine Optimum Lunette Load for the Lance Lightweight Launcher
1963
87 pages
Report
No indication
English
Missile Launching & Support Systems , Road Transportation , Guided missile launchers , Tow bars , Loads(Forces) , Optimization , Towing vehicles , Dynamics , Braking , Human factors engineering , Handling , Response , Structural properties , Force(Mechanics) , Acceleration , Ground speed , Deflection , Mathematical models , Surface to surface missiles , Lance missiles , Stopping distance
Lance Missile Launcher Stability Tests
NTIS | 1967
|Montre pourvue d'une lunette tournante avec système de verrouillage de la lunette.
European Patent Office | 2020
|