Experimentally determined rocket-exhaust flowfield in a constrictivetube launcher

• 1 December 1975
• journal article
• Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
• Vol. 12  (12) , 711-717
• https://doi.org/10.2514/3.27869

Abstract

Keywords

• EXPERIMENTALLY DETERMINED
• DETERMINED ROCKET
• CONSTRICTIVETUBE LAUNCHER
• ROCKET EXHAUST
• EXHAUST FLOWFIELD