Titan IV - An integrated spacecraft/booster view

Physics

Scientific paper

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Contractors, Government Procurement, Payload Integration, Spacecraft Design, Titan Launch Vehicles, Mission Planning, Orbit Insertion, Project Management, Titan Icbm, Titan Project

Scientific paper

The Titan IV launch vehicle is briefly described focusing on the integration process which starts with spacecraft environmental and mechanical interface requirements definition and progresses through physical mating of the spacecraft and launch vehicle, launch countdown, launch, and orbit insertion. An approach to payload integration is presented where teamwork between the government and contractor organizations provides the framework necessary for the efficient incorporation of mission unique requirements.

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