Details of X-15 arrangement and flight control system; aerodynamic surfaces for control consist of upper and lower verticals; trailing edges of upper and lower fixed portions deflect as speed brakes; reaction control rockets are located in nose for pitch and yaw and at wing tips for roll; propellant supply system; evaluation and test data obtained on flight control system; current status of flight test program; expected performance capabilities. (See also SAE -- Paper n S-247 for meeting v 68 n 8 Mar 24 1960 9 p)
X-15 -- Reaction control aircraft
SAE -- J
1960
4 pages
Aufsatz (Zeitschrift)
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
X-15 -- Reaction control aircraft
Engineering Index Backfile | 1960
|Reaction Control Systems for V/STOL Aircraft
SAE Technical Papers | 1965
|THE X-15-A REACTION CONTROL AIRCRAFT
SAE Technical Papers | 1960
|Reaction control system augmentation for V/STOL aircraft
NTRS | 1979
|