An attitude control system for large launch vehicles.
- 1 June 1969
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 6 (6) , 748-751
- https://doi.org/10.2514/3.29653
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- Load-reducing flight control systems for the Saturn V with various payloadsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1968
- An acceleration vector attitude control system.Journal of Spacecraft and Rockets, 1968