Effect of airframe geometry on thrust performance of aerospace plane

2000 ◽  
Author(s):  
Masatoshi Kodera ◽  
Takeshi Kanda ◽  
Kouichiro Tani
Keyword(s):  
Aerospace Plane ◽  
Thrust Performance

Some aspects of design of the heat-shielding of an aerospace plane with power increase for the flying device

2007 ◽  
Vol 13 (1) ◽  
pp. 29-36
Author(s):  
A.S. Levenko ◽  
◽  
V.I. Kukushkin ◽  
A.V. Sichevoy ◽  
◽  
...  
Keyword(s):  
Power Increase ◽  
Heat Shielding ◽  
Aerospace Plane

scholarly journals Thrust Performance of Rotary-Valved Four-Cylinder Pulse Detonation Rocket Engine

2015 ◽  
Vol 58 (4) ◽  
pp. 193-203 ◽  
Author(s):  
Ken MATSUOKA ◽  
Ryuki SAKAMOTO ◽  
Tomohito MOROZUMI ◽  
Jiro KASAHARA ◽  
Akiko MATSUO ◽  
...  
Keyword(s):  
Rocket Engine ◽  
Pulse Detonation ◽  
Pulse Detonation Rocket Engine ◽  
Thrust Performance

A Study on Thrust Performance of Counter-Rotating Biomimetic Propeller System for a Manned Drone

2021 ◽  
Vol 24 (1) ◽  
pp. 41-46
Author(s):  
Soo-Jung Kim ◽  
Tae-Young Yeom ◽  
Seungbae Lee
Keyword(s):  
Thrust Performance

scholarly journals Effects of Nozzle Geometries on Thrust Performance Improvement of Micro-Multi-Nozzle-Array Thrusters

2009 ◽  
Vol 7 (ists26) ◽  
pp. Pb_77-Pb_82
Author(s):  
Fujimi SAWADA ◽  
Atsushi KOSHIYAMA ◽  
Shuji HAGIWARA ◽  
Hideyuki HORISAWA ◽  
Ikkoh FUNAKI
Keyword(s):  
Performance Improvement ◽  
Nozzle Geometries ◽  
Thrust Performance

HTHL Space Vehicles: Concepts and Control Problems

2014 ◽  
Vol 629 ◽  
pp. 382-387
Author(s):  
Alexander Nebylov
Keyword(s):  
Control Systems ◽  
Ground Effect ◽  
Easy Access ◽  
Space Vehicles ◽  
Space Launch ◽  
Design Requirements ◽  
Last Stage ◽  
Launch Systems ◽  
And Control ◽  
Aerospace Plane

Integrated launch systems that include aerospace plane (ASP) and another heavy winged vehicle (plane or better Wing-in-Ground effect vehicle) as a booster are reviewed. It is shown that WIG-vehicle with a mass of 1500 ton or more is capable to carry ASP with initial mass of 500 ton and landing mass of 60-70 ton. Ekranoplane can provide ASP with the primary speed of Mach 0.5-0.65 in the required direction that allows lowering the design requirements to ASP's wing area and engines. A number of other advantages from the offered transport system are linked to possible use of WIG-vehicle at ASP landing. Heavy WIG-vehicle is unique vehicle for realizing the progressive idea of docking to descending ASP, allowing expanding opportunities of its landing. The problem of ASP horizontal landing without undercarriage by docking with other flying vehicle at the last stage of decent and the requirements to control systems for relative motion control of both vehicles are discussed. The progressive idea of joining space launch technologies with marine technologies is developed. It is especially important for countries with strongly limited areas of land territory but with easy access to the ocean.

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