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.


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    TITAN 3 AND TITAN 4 SPACE LAUNCH VEHICLES

    Richards, G.R. | Online Contents | 1993


    The Titan IV launch Vehicle

    Morrissey, Arthur C. / O'Neill, Stephen T. | SAE Technical Papers | 1989


    The commercial Titan launch vehicle

    TROUTMAN, J. / ISAKOWITZ, S. | AIAA | 1987