Avatar is projected to weigh 25 tons, of which 60% of that mass would be liquid hydrogen fuel.[1] The oxygen required by the vehicle for combustion in outer space would be collected from the atmosphere during takeoff, thus reducing the need to carry oxygen during launch.[1] The notional specification is for a payload weighing up to 1,000 kg (2,200 lb) to low Earth orbit and to withstand up to 100 launches and reentries.[2][1]
If built, Avatar would take off horizontally like a conventional airplane from a conventional airstrip using turbo-ramjet engines that burn hydrogen and atmospheric oxygen.[1] During this cruising phase, an on-board system would collect air from the atmosphere, from which liquid oxygen would be separated and stored and used to burn the stored hydrogen in the final flight phase to attain orbit. The vehicle would be designed to permit at least one hundred launches and atmospheric reentries.[1]
Feasibility study
The Avatar concept study was commissioned by India's Defence Research and Development Organisation in 2001.[2] India's Space Agency ISRO has no connection with the project.[4][5][6] Air Commodore Raghavan Gopalaswami, who headed the study, made a presentation on the spaceplane at the global conference on propulsion at Salt Lake City, United States on July 10, 2001.[2][1][7]
See also
Spaceplanes of comparable role, configuration and era
^"AVATAR- Hyper Plane to be built by INDIA". India's Military and Civilian Technological Advancements. December 19, 2011.
^ ab"Government of India Department of Space"(PDF). March 14, 2012. Archived from the original(PDF) on August 5, 2016. Retrieved 2016-04-27. Feasibility study of project "AVATAR)" has been done by a group of scientists in DRDO. ISRO has no connection with the project.