Research Catalog

Optimal pitch thrust-vector angle and benefits for all flight regimes

Title
Optimal pitch thrust-vector angle and benefits for all flight regimes / Glenn B. Gilyard, Alexander Bolonkin.
Author
Gilyard, Glenn B.
Publication
Edwards, California : National Aeronautics and Space Administration, Dryden Flight Research Center, March 2000.

Available Online

https://purl.fdlp.gov/GPO/gpo85803

Details

Additional Authors
  • Bolonkin, Alexander
  • Hugh L. Dryden Flight Research Center, issuing body.
Description
1 online resource (22 pages) : illustrations.
Series Statement
NASA/TM ; 2000-209021
Uniform Title
NASA technical memorandum ; 2000-209021.
Subject
  • Pitch (inclination)
  • Thrust vector control
  • Automatic flight control
  • Angles (geometry)
Note
  • "March 2000."
  • "Performing organization: NASA Dryden Flight Research Center"--Report documentation page.
Bibliography (note)
  • Includes bibliographical references (page 22).
Type of Report (note)
  • Technical memorandum.
Funding (note)
  • Sponsored by the National Aeronautics and Space Administration
Source of Description (note)
  • Description based on online resource; title from PDF title page (NASA, viewed Oct. 23, 2017).
Call Number
GPO Internet NAS 1.15:209021
OCLC
marcive858246018
Author
Gilyard, Glenn B., author.
Title
Optimal pitch thrust-vector angle and benefits for all flight regimes / Glenn B. Gilyard, Alexander Bolonkin.
Publisher
Edwards, California : National Aeronautics and Space Administration, Dryden Flight Research Center, March 2000.
Type of Content
text
Type of Medium
computer
Type of Carrier
online resource
Series
NASA/TM ; 2000-209021
NASA technical memorandum ; 2000-209021.
Bibliography
Includes bibliographical references (page 22).
Type Of Report
Technical memorandum.
Funding
Sponsored by the National Aeronautics and Space Administration WU 522-16-14-00-39-00-LIO H-2402
Connect to:
https://purl.fdlp.gov/GPO/gpo85803
Added Author
Bolonkin, Alexander, author.
Hugh L. Dryden Flight Research Center, issuing body.
Other Form:
Print version: Gilyard, Glenn B. Optimal pitch thrust-vector angle and benefits for all flight regimes (OCoLC)45534249
Microfiche version: Gilyard, Glenn B. Optimal pitch thrust-vector angle and benefits for all flight regimes (OCoLC)45009655
Gpo Item No.
0830-D (online)
Sudoc No.
NAS 1.15:209021
View in Legacy Catalog