NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Experiments on the dynamic stability of the space shuttleSome dynamic stability experiments on the space shuttle using a half-model oscillatory technique are discussed. Resulting information from the experiments is presented and includes: (1) dynamic pitching characteristics of both the orbiter and the booster alone as well as of the two models mated into a single launch configuration; (2) the static and dynamic interference effects during an abort separation maneuver; and (3) the dynamic plume interference effect.
Document ID
19720013228
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Orlik-Rueckermann, K. J. (National Research Council of Canada Ottawa Ontario, Canada)
Laberge, J. G. (National Research Council of Canada Ottawa Ontario, Canada)
Hanff, E. S. (National Research Council of Canada Ottawa Ontario, Canada)
Date Acquired
August 6, 2013
Publication Date
February 1, 1972
Publication Information
Publication: NASA. Langley Res. Center Space Shuttle Aerothermodyn. Technol. Conf., vol. 3
Subject Category
Space Vehicles
Accession Number
72N20878
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

IDRelationTitle19720013221Collected WorksSpace Shuttle Aerothermodynamics Technology Conference. Volume 3: AerodynamicsN72-20871 11-31Collected Works
No Preview Available