Helicon engine in outboard air as a successful solution for maintaining small space vehicle in orbits up to 200 km-Reference-Cited by-同舟云学术

Helicon engine in outboard air as a successful solution for maintaining small space vehicle in orbits up to 200 km

Published:2019 Issue: Volume: Page:
ISSN:0094-243X
Container-title:XLIII ACADEMIC SPACE CONFERENCE: dedicated to the memory of academician S.P. Korolev and other outstanding Russian scientists – Pioneers of space exploration
language:
Short-container-title:

Author:

Shumeiko A. I.,Telekh V. D.

Publisher

AIP Publishing

Link

http://aip.scitation.org/doi/pdf/10.1063/1.5133330

Reference20 articles.

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2. DePasquale, D., Charania, A., “Nano/Microsatellite Launch Demand Assessment 2011”, Revision A, 22 November 2011. www.spaceworkscommercial.com.

3. Kim, V., & Semenkin, A. (1996). Evaluation of low power Hall thruster propulsion. In AIAA, ASME, SAE and ASEE Joint Propulsion Conference and Exhibit (Vol. 32, pp. 1–3).

4. Proposals for the construction of space systems based on small spacecraft and a transport and power module with a nuclear power plant

5. Protasov, Y., Protasov, Y., & Telekh, V. (2000). Laser propulsion-Radiative gasdynamic and thermophysical interchamber processes of double-stage laser rocket thruster. I. In 36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit (p. 3485).

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