This report covers the 'B' series launcher release tests. Two simulated missile launches of 10 inches free travel were made at a thrust/weight (T/W) ratio of 1.33 and two simulated missile launches of 11 inches free travel were made at a thrust/weight (T/W) ratio of 1.48. These tests were also used as the dynamic check-out for the 'B' series release curves. (Author)
'B' Series Launcher Release Tests
1959
81 pages
Report
Keine Angabe
Englisch
Missile Launching & Support Systems , Missile Technology , Guided missile launchers , Performance(Engineering) , Release mechanisms , Surface to surface missiles , Launching , Simulation , Thrust , Weight , Pressure , Reliability , Attenuation , Damage assessment , Structural members , Loads(Forces) , Seals , Leakage(Fluid) , Pneumatic devices , Pipes , Shafts(Machine elements) , Hydraulic equipment , Umbilical cords(Aerospace) , Disconnect fittings , Shock absorbers , Bushings , Fracture(Mechanics) , Deformation , Atlas , Xsm-65b missiles
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