Gas-phase nuclear rocket engines and propulsive mass for them.
- Paper number
IAC-15,C4,IP,8,x28275
- Author
Mr. Oleg Aleksandrov, AVIASTAR Inc www.aviastar.us, United States
- Year
2015
- Abstract
Gas-phase nuclear rocket rocket engines and propulsive mass for them. In this report schemes and methods of creation of gas-phase rocket engines by which propulsive mass for exhaust will be offered usual soil of celestial bodies is. Regolith, sand, stones, ice and so forth. This type of engines won't be replaceable at active development of distant planets and asteroids of solar system both in automatic and in piloted the modes. The author pays much attention to absolute safety of an exit of such engines in space and their operation.
- Abstract document
- Manuscript document
IAC-15,C4,IP,8,x28275.pdf (🔒 authorized access only).
To get the manuscript, please contact IAF Secretariat.