Supersonic Flight Separation Simulation for TSTO Launch Vehicles Considering Shock Wave Interaction Reduction
50th, Aerospace sciences meeting; including the new horizons forum and aerospace exposition 2012 ; 2012 ; Nashville, TN
Aerospace sciences meeting; including the new horizons forum and aerospace exposition 2012 ; 3695-3705
2012-01-01
11 pages
Includes bibliographical references and index
Conference paper
English
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
TSTO Reusable Launch Vehicles Using Airbreathing Propulsion
British Library Conference Proceedings | 2006
|Cost-Optimized Stage Separation Velocity of Winged TSTO Launch Vehicles
British Library Conference Proceedings | 1994
|