The report was prepared to document the results of initial studying and testing of an Atlas fly-out launcher system. Specifically the thermodynamic, gas dynamic and acoustical effects on the missile, launcher and launcher equipment were studied to evaluate the system. (Author)
Atlas 'E' Series Fly-out Launcher Study
1968
76 pages
Report
No indication
English
Missile Launching & Support Systems , Missile Technology , Surface to surface missiles , Guided missile silos , Launching , Feasibility studies , Models(Simulations) , Gas flow , Exhaust gases , Deflection , Booster rockets , Sustainer engines , Flame deflectors , Ducts , Configuration , Design , Acoustic properties , Failure , Noise , Fatigue(Mechanics) , Damage , Reliability , Vibration , Resonance , Atlas , Xsm-65e missiles
NTIS | 1969
|NTRS | 1969
|NTRS | 1967
|SILO LIFT LAUNCHER SYSTEM FOR THE ATLAS ICBM
SAE Technical Papers | 1960
|'B' Series Launcher Release Tests
NTIS | 1959
|