Problem of automatic stabilization system for rocket with high altitude nearly vertical trajectory; flight path solved by employing three separate subsystems: (1) motor control system which obtains corrective moments by altering line of thrust of liquid rocket engine, (2) aerodynamic roll system employs movable tabs attached to two of fins, and (3) thrust reaction system which obtains control moments through use of small jet motors.
Development of stabilization system for viking rocket
Jet Propulsion
Jet Propulsion ; 25 , n 8 ; p 392-395 + 399
1955
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Engineering Index Backfile | 1952
|GWLB - Gottfried Wilhelm Leibniz Bibliothek | 1955
|Photography from Viking II rocket
Engineering Index Backfile | 1955
|NTRS | 1977
|Coordinated Viking and sounding rocket studies
Elsevier | 1989
|