A realistic concept of a manned Mars mission with nuclear–electric propulsion-Reference-Cited by-同舟云学术

A realistic concept of a manned Mars mission with nuclear–electric propulsion

Published:2015-11 Issue: Volume:116 Page:299-306
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Loeb H.W.,Petukhov V.G.,Popov G.A.,Mogulkin A.I.

Funder

Russian Ministry of Education and Science

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference14 articles.

1. Human Exploration to Mars – Design Reference Architecture 5.0, July 2009; NASA-SP-2009-566.

2. Ion Propulsion for Space Flight;Stuhlinger,1964

3. Electric Propulsion

4. Performance parameters for electric-propulsion systems.

5. H.W. Loeb and X. Da, Large scale radio-frequency ion thrusters for manned Mars missions, in: Proceedings of the 43rd International Astronautical Congress IAF-92-0619, Dresden, 1990.

Cited by 9 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. An approach for end-to-end optimization of low-thrust interplanetary trajectories using collinear libration points;Acta Astronautica;2024-08

2. Spacecraft Medium Voltage Direct-Current (MVDC) Power and Propulsion System;Electronics;2024-05-07

3. Experimental study of heat rejection performance of water membrane evaporator in vacuum environment;Applied Thermal Engineering;2024-02

4. Optimization of a Low-Thrust Heliocentric Trajectory between the Collinear Libration Points of Different Planets;Cosmic Research;2023-09-16

5. Optimization of a Low-Thrust Heliocentric Trajectory between the Collinear Libration Points of Different Planets;Космические исследования;2023-09-01