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Combined High and Low Thrust Propulsion for Fast Piloted Mars Missions
Language: en
Pages: 30
Authors: National Aeronautics and Space Administration (NASA)
Categories:
Type: BOOK - Published: 2018-08-16 - Publisher: Createspace Independent Publishing Platform

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The mission benefits of using both high thrust nuclear thermal propulsion (NTP) and low acceleration, high specific impulse nuclear electric propulsion (NEP) to
Combined High and Low Thrust Propulsion for Fast Piloted Mars Missions
Language: en
Pages: 16
Authors:
Categories:
Type: BOOK - Published: 1992 - Publisher:

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Fast Interplanetary Missions with Low-thrust Propulsion Systems
Language: en
Pages: 40
Authors: W. E. Moeckel
Categories: Propulsion systems
Type: BOOK - Published: 1961 - Publisher:

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A simple family of indirect-transfer trajectories between circular orbits is used to evaluate the mass ratio required to complete round-trip interplanetary miss
Fast Interplanetary Missions with Low-thrust Propulsion Systems
Language: en
Pages: 29
Authors: W. E. Moeckel
Categories: Propulsion systems
Type: BOOK - Published: 1961 - Publisher:

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A simple family of indirect-transfer trajectories between circular orbits is used to evaluate the mass ratio required to complete round-trip interplanetary miss
Advanced Hybrid Nuclear Propulsion Mars Mission Performance Enhancement
Language: en
Pages: 4
Authors:
Categories:
Type: BOOK - Published: 1992 - Publisher:

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Nuclear electric propulsion (NEP), compared with chemical and nuclear thermal propulsion (NTP), can effectively deliver the same mass to Mars using much less pr