The objective of the demonstration test program was to confirm the validity of the new component designs by engine tests at both nominal and extreme Titan IIIM operating conditions without unnecessarily repeating the Titan II and Titan III qualification tests. The test program also served as a convenient vehicle for testing related items, not intrinsic to the engine system, such as the Martin POGO accumulators, gimbal actuators, flight instrumentation, and ground equipment. The planned program consisted of 30 tests, 15 on each of two engines.
Titan IIIM Standard Space Launch Vehicle Development Report for the Stage I Engine Demonstration Testing
1969
525 pages
Report
Keine Angabe
Englisch
Rocket Engines & Motors , Space Launch Vehicles & Support Equipment , Launch vehicles , Booster rockets , Captive tests , Liquid propellant rocket engines , Ablation , Combustion chambers , Fuel injectors , Gas generating systems , Extendable structures , Design , Turbopumps , Redundant components , Performance(Engineering) , Nozzle gas flow , Manned spacecraft , Titan 3m missiles , 624a program , Ablative skirts , Lr-87 engines , Manned orbital laboratory , Mol(Manned orbital laboratory) , Over expanded nozzle flow , Skirts , Titan 3 , Transtages
TITAN 3 AND TITAN 4 SPACE LAUNCH VEHICLES
Online Contents | 1993
|SAE Technical Papers | 1989
|The commercial Titan launch vehicle
AIAA | 1987
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