NDLI: Astp (sa-210) launch vehicle operational flight trajectory dispersion analysis, volume 1

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Astp (sa-210) launch vehicle operational flight trajectory dispersion analysis, volume 1

Content Provider	NASA Technical Reports Server (NTRS)
Author	Ransom, F. A. Williams, N. D. Klug, G. W.
Copyright Year	1975
Description	In order to establish realistic deviation limits for the ASTP (SA-210) Launch Vehicle Operational Flight Trajectory, a dispersion analysis was conducted. The nominal trajectory prescribed for this analysis is the ASTP (SA-210) Launch Vehicle 500 Pound Launch Window Opening OT. The error sources considered are those associated with predictions of vehicle characteristics, vehicle systems performance, and flight environment. The nominal vehicle, the boost trajectory simulations, the error sources, the analytic procedures utilized, and the results are discussed. Launch vehicle guidance system inaccuracies were determined from the guidance error analysis. These data are composed of individual error source trajectory parameter dispersion envelopes.
File Size	2516992
Page Count	79
File Format	PDF
Alternate Webpage(s)	http://archive.org/details/NASA_NTRS_Archive_19760004113
Archival Resource Key	ark:/13960/t3809vz1w
Language	English
Publisher Date	1975-04-04
Access Restriction	Open
Subject Keyword	Astrodynamics Spacecraft Guidance Apollo Soyuz Test Project Launch Vehicles Error Analysis Trajectory Analysis Launch Windows Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science
Content Type	Text
Resource Type	Technical Report

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