Back to Search Start Over

Analysis of a Radioisotope Thermal Rocket Engine

Authors :
Machado-Rodriguez, Jonathan P
Landis, Geoffrey A
Publication Year :
2017
Publisher :
United States: NASA Center for Aerospace Information (CASI), 2017.

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

Subjects :
Spacecraft Propulsion And Power

Details

Language :
English
Database :
NASA Technical Reports
Notes :
WBS 469947.03.03.01
Publication Type :
Report
Accession number :
edsnas.20170006624
Document Type :
Report