Computer Science – Sound
Scientific paper
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.
No associations
LandOfFree
Launch vehicle reliability and launch availability relationships resulting from winds-aloft launch constraints does not yet have a rating. At this time, there are no reviews or comments for this scientific paper.
If you have personal experience with Launch vehicle reliability and launch availability relationships resulting from winds-aloft launch constraints, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Launch vehicle reliability and launch availability relationships resulting from winds-aloft launch constraints will most certainly appreciate the feedback.
Profile ID: LFWR-SCP-O-1774920