WebAbstract. This paper discusses the current R&D status and plans concerning a Mach 6 turbojet engine with an air-precooling system for the first stage of a two-stage-to-orbit space plane (TSTO). An air-turbo ramjet engine with the expander-cycle (ATREX) has been designed and tested at sea level static conditions, which demonstrated the engine ... Web10th AIAA/NAL-NASDA-ISAS International Space Planes and Hypersonic Systems and Technologies Conference

New indian hypersonic jet engine :india to America in 90 min, tsto ...

WebFeb 1, 2001 · The optimal Mach number for staging the second stage of the TSTO spaceplane (with air-breathing propulsion on the first stage) is 10, based on life-cycle cost … WebMay 23, 2016 · But my modded spaceplane gets to orbit now with 89 oxidizer and 280 LF remaining to do your rendezvous and land with. It still flies OK in atmosphere and reenters … cz of menzis

Aerodynamic analysis of a TSTO spaceplane — University of …

WebJan 1, 1997 · ATREX development study has been conducted with the sea level static tests since 1990. ATREX engine for tests is the scaled model designated by "ATREX-500" of which fan inlet diameter is 300 mm and overall length 2,200 mm. From 1992 have been performed the wind tunnel tests on the primary aerodynamic components such as the axisymmetric … WebDec 21, 2005 · Design aspects of a small pre-cooled turbojet engine for flight experiments are investigated in this study. Pre-cooled turbojet engine is a hypersonic engine suitable for Two Stage To Orbit (TSTO) Space Planes and other hypersonic cruise vehicles. The engine has a capability to accelerate vehicles with a flight speed range between Mach 0 and 6. … WebDec 1, 2001 · Abstract. An expander cycle air-turbo ramjet (ATREX) engine has been developed in the Institute of Space and Astronautical Science (ISAS). The ATREX will be … bing has the most ads search engine