Optimal pitch thrust-vector angle and benefits for all flight regimes
By: Glenn B. Gilyard, Alexander Bolonkin.
Contributors: Bolonkin, Alexander.; NASA Dryden Flight Research Center.
Series: [NASA technical memorandum] -- NASA/TM-2000-209021.; NASA technical memorandum -- 209021.
Publisher: National Aeronautics and Space Administration, Dryden Flight Research Center; National Technical Information Service, distributor
Published: 2000
Place of publication: Edwards, Calif; [Springfield, Va
Language: eng
Format: Microform
Subjects: Pitch (Inclination); Thrust vector control.; Automatic flight control.; Angles (geometry)
Other titles: Optimal pitch thrust vector angle and benefits for all flight regimes.
Notes: Shipping list no.: 2000-0886-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 2000] 1 microfiche.