Conceptual Design of an Air-Breathing Electric Thruster for CubeSat Applications-Reference-Cited by-同舟云学术

Conceptual Design of an Air-Breathing Electric Thruster for CubeSat Applications

Published:2018-05 Issue:3 Volume:55 Page:632-639
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Jackson Stephen W.¹,Marshall Robert¹

Affiliation:

1. University of Colorado, Boulder, Colorado 80305

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.A33993

Reference12 articles.

1. ConleyB. R. “Utilization of Ambient Gas as a Propellant for Low Earth Orbit Electric Propulsion,” M.S. Thesis, Massachusetts Inst. of Technology, Cambridge, MA, 1995.

2. A review of research in low earth orbit propellant collection

3. McGuireT. J. “Aero-Assisted Orbital Transfer Vehicles Utilizing Atmosphere Ingestion,” M.S. Thesis, Massachusetts Inst. of Technology, Cambridge, MA, 2001.

4. NRLMSISE-00 empirical model of the atmosphere: Statistical comparisons and scientific issues

5. Analysis of the orbital decay of spherical satellites using different solar flux proxies and atmospheric density models

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