NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Research on development of equations for performance trajectory computationA computer program for computing the performance trajectory of spacecraft was developed. An analytical study of a minimum fuel flight for high speed aircraft was conducted. The computer program to compute a minimum time reentry into the atmosphere for an Apollo-type capsule is presented. A technical summary of the minimum fuel problem is provided.
Document ID
19740023190
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Harmon, G. R. (Auburn Univ. AL, United States)
Date Acquired
August 7, 2013
Publication Date
January 1, 1974
Publication Information
Publication: Multivariant Function Model Generation
Subject Category
Space Sciences
Accession Number
74N31303
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Document Inquiry

Available Downloads

There are no available downloads for this record.

Related Records

IDRelationTitle19740023186Collected WorksMultivariant function model generation
No Preview Available