Optimal payload trajectory characteristics for horizontally launchedbooster vehicle.
- 1 February 1968
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 5 (2) , 218-220
- https://doi.org/10.2514/3.29222
Abstract
No abstract availableKeywords
This publication has 1 reference indexed in Scilit:
- Nuclear-thermal vs chemical drives for superorbital velocitiesJournal of Spacecraft and Rockets, 1964