NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Post-ejection impacts of the space shuttle solid rocket booster nose capThe dynamics of impacts between the nose cap ejected from the space shuttle solid rocket booster and the drogue parachute pack are analyzed. The analysis is restricted to planar impact, and assumes the law of restitution and the possible occurrence of three types of impact, depending on the friction behavior of the colliding surfaces: forward slip; backward slip; no slip (normal rebound). The positions of both bodies and their velocities at the time of impact are required. Seven successive impacts, representing all three types, detected and simulated for the case of nose cap ejection at 20 fps normal to the direction of airflow, with selected coefficients of friction (0.25) and restitution (0.85).
Document ID
19760033202
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Banerjee, A. K.
(Northrop Services, Inc. Huntsville, AL, United States)
Coppey, J. M.
(Northrop Services, Inc. Huntsville, Ala., United States)
Date Acquired
August 8, 2013
Publication Date
October 1, 1975
Publication Information
Publication: Journal of Spacecraft and Rockets
Volume: 12
Subject Category
Astrodynamics
Accession Number
76A16168
Funding Number(s)
CONTRACT_GRANT: NAS8-21810
Distribution Limits
Public
Copyright
Other

Available Downloads

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