Monitoring techniques for the X-29A aircraft's high-speed rotating power takeoff shaft
By: David F. Voracek.
Contributors: Dryden Flight Research Facility.
Series: NASA technical memorandum -- 101731.
Publisher: National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility; For sale by the National Technical Information Service]
Published: 1990
Place of publication: Edwards, Calif; [Springfield, Va
Language: eng
Format: Microform
Number of pages: 21
Subjects: Grumman X-29A (Jet plane) -- Testing.; Engine failure.; Flight operations.; Graphite-epoxy composites.; Ground operational support system.; High speed.; Rotating shafts.; Takeoff.; Vibration.; X-29 aircraft.
Notes: Shipping list no.: 91-0796-M.

"December 1990"--Cover.

"Performing organization report no.: H-1680"--Tech. rept. documentation p.

Includes bibliographical references (p. 7).

Also available via Internet from the NASA Technical Report Server web site. Address as of 2/17/05: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19910009768%5F1991009768.pdf; current access available via PURL.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1991]. 1 microfiche : negative.

RTOP 533-02-51.