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Program For Simulating Dynamics Of Aerospace VehiclesSORT (Simulation and Optimization of Rocket Trajectories) is general-purpose three-degree-of-freedom with three axis static moment balance simulation of flight dynamics of arbitrary aerospace vehicle. Modular structure facilitates application to variety of trajectory-analysis problems. Contains math model of aerodynamics completely generalized. Computes both longitudinal and lateral forces and moments. In addition to fore-body coefficients, computes longitudinal base effect aerodynamic forces and moments. Simplified ballistic-coefficient model also available for analysis of ballistic entry. Written using ANSI FORTRAN 77.
Document ID
19950065520
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Berning, M. J. (Lockheed Engineering and Sciences Co.)
Sagis, K. D. (Lockheed Engineering and Sciences Co.)
Date Acquired
August 17, 2013
Publication Date
August 1, 1995
Publication Information
Publication: NASA Tech Briefs
Volume: 19
Issue: 8
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
MSC-22496
MSC-22498
MSC-22497
Accession Number
95B10361
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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