NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Due to the lapse in federal government funding, NASA is not updating this website. We sincerely regret this inconvenience.

Back to Results
Six degrees of freedom equations of motion and trajectory equations of a rigid fin stabilized missile with variable mass
Document ID
19740074646
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Donegan, J. J.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 7, 2013
Publication Date
January 1, 1958
Publication Information
Publication: Notes Space Technol.
Subject Category
General
Accession Number
74N72585
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Document Inquiry

Available Downloads

There are no available downloads for this record.
No Preview Available