Thrust Calculation for Low-Reynolds-Number Micronozzles-Reference-Cited by-同舟云学术

Thrust Calculation for Low-Reynolds-Number Micronozzles

Published:2017-01 Issue:1 Volume:54 Page:287-298
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Pearl J. M.¹,Louisos W. F.¹,Hitt D. L.¹

Affiliation:

1. University of Vermont, Burlington, Vermont 05405

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.A33535

Reference35 articles.

1. MuellerJ. “Thruster Options for Microspacecraft: A Review and Evaluation of Existing Hardware and Emerging Technologies,” AIAA Paper 1997-3058, July 1997.

2. MEMS-based satellite micropropulsion via catalyzed hydrogen peroxide decomposition

3. BaytR. L.BreuerK. S. “Systems Design and Performance of Hot and Cold Supersonic Microjets,” AIAA Paper 2001-0721, Jan. 2001.

4. Development of a Thrust Stand Micro-Balance to Assess Micropropulsion Performance

5. BlackW. N. “Performance Measurements of Low Reynolds Number Nozzle Geometries,” M.S. Thesis, Dept. of Mechanical and Aerospace Engineering, Univ. of Colorado, Colorado Springs, CO, 2011.

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