Innovative concepts for the Titan II space launch vehicle

Details Innovative concepts for the Titan II space launch vehicle Innovative concepts for the Titan II space launch vehicle

Jun 1991

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1991jpsc.confq....f&link_type=abstract

AIAA, SAE, ASME, and ASEE, Joint Propulsion Conference, 27th, Sacramento, CA, June 24-26, 1991. 9 p.

Physics

Hypergolic Rocket Propellants, Titan Launch Vehicles, Titan 2 Icbm, Attitude Control, Booster Rocket Engines, Inertial Guidance, Solid Propellant Rocket Engines, Transfer Orbits

Scientific paper

A number of concepts that will enable Titan II to launch a greater spectrum of payloads is presented. The history of Titan development is outlined, and emphasis is placed on the development of the Titan II space launch vehicle (SLV) as well as on two types of missions contracted for the Titan II SLV. The current payload capabilities of the Titan II SLV are discussed, and attention is focused on a Titan II variant called the Titan IIS with a number of solid rocket motors added to the first stage, the Titan IIL employing liquid rocket boosters, and an enhanced attitude control system. A concept involving two small bipropellant engines on the aft end of stage II as well as a concept involving restarting of the stage-II main engine are considered.

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