Launch vehicle reliability and launch availability relationships resulting from winds-aloft launch constraints

Details Launch vehicle reliability and launch availability relationships resulting from winds-aloft launch constraints Launch vehicle reliability and launch availability relationships resulting from winds-aloft launch constraints

Jan 1993

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1993aiaa.meetss...s&link_type=abstract

AIAA, Aerospace Sciences Meeting and Exhibit, 31st, Reno, NV, Jan. 11-14, 1993, 15 p.

Computer Science

Sound

Launch Windows, Spacecraft Reliability, Titan Launch Vehicles, Winds Aloft, Aerodynamic Loads, Angle Of Attack, Balloon Sounding, Prelaunch Tests, Spacecraft Guidance

Scientific paper

To insure an adequate level of vehicle reliability, wind-aloft constraints for the Titan IV launch vehicle have been developed. Equations have been derived for vehicle capability, vehicle reliability, launch availability, and winds-aloft launch constraint correlation to determine mathematical relationships between launch vehicle reliability and launch availability. These equations give quantifiable values of vehicle reliability and launch availability that can be used to optimize the winds-aloft launch constraint system.

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