Titan improvement study - Hydrogen core stages

Details Titan improvement study - Hydrogen core stages Titan improvement study - Hydrogen core stages

Jun 1991

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1991jspro..28..356m&link_type=abstract

Journal of Spacecraft and Rockets (ISSN 0022-4650), vol. 28, May-June 1991, p. 356-358.

Computer Science

Performance

Hydrogen Oxygen Engines, Titan Launch Vehicles, Upper Stage Rocket Engines, Earth Orbital Environments, Geosynchronous Orbits, Interplanetary Flight, Manned Space Flight, Unmanned Spacecraft

Scientific paper

The performance benefits and comparative cost-effectiveness of Titan/Centaur launcher improvement options involving a new LH2/LOX second stage and/or a new LH2/LOX first stage are presented. This incremental improvement approach involves higher confidence due to high components-commonality with well-tested systems. The proposed second stage's capabilities are such as to allow it to serve as an OTV. This improvement to Titan constitutes one of several justifications for a new 500-1000 kN thrust liquid-fuel engine.

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