United Trajectory Design Method for Return to Launch Site of Suborbital Reusable Launch Vehicle (AIAA 2017-2108)
AIAA Interantional Space Planes and Hypersonic Systems and Technologies (Conference)
2017-01-01
9 pages
Conference paper
English
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
British Library Conference Proceedings | 2017
|Concept Study of a Reusable Suborbital Launch Vehicle (AIAA 2018-0084)
British Library Conference Proceedings | 2018
|Design and Optimization of RBCC Powered Suborbital Reusable Launch Vehicle (AIAA 2014-2361)
British Library Conference Proceedings | 2014
|Return and Abort Trajectory Optimisation for Reusable Launch Vehicles (AIAA 2017-2250)
British Library Conference Proceedings | 2017
|