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Analysis of a Radioisotope Thermal Rocket Engine
- Publication Year :
- 2017
- Publisher :
- United States: NASA Center for Aerospace Information (CASI), 2017.
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Abstract
- The Triton Hopper is a concept for a vehicle to explore the surface of Neptunes moon Triton, which uses a radioisotope heated rocket engine and in-situ propellant acquisition. The initial Triton Hopper conceptual design stores pressurized Nitrogen in a spherical tank to be used as the propellant. The aim of the research was to investigate the benefits of storing propellant at ambient temperature and heating it through a thermal block during engine operation, as opposed to storing gas at a high temperature.
- Subjects :
- Spacecraft Propulsion And Power
Subjects
Details
- Language :
- English
- Database :
- NASA Technical Reports
- Notes :
- WBS 469947.03.03.01
- Publication Type :
- Report
- Accession number :
- edsnas.20170006624
- Document Type :
- Report