Solid-propellant pulsed plasma microthruster studies-Reference-Cited by-同舟云学术

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Solid-propellant pulsed plasma microthruster studies

Published:1968-01-22 Issue: Volume: Page:
ISSN:
Container-title:6th Aerospace Sciences Meeting
language:
Short-container-title:

Author:

GUMAN W.¹,PEKO P.²

Affiliation:

1. FAIRCHILD HILLER CORP., REPUBLIC AVIATION DIV., POWER CONVERSION DEPT., FARMINGDALE, N.Y.

2. USAF, SYSTEMS COMMAND, RESEARCH AND TECHNOLOGY DIV., AERO PROPULSION LAB., WRIGHT-PATTERSON AFB, OHIO

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1968-85

Reference29 articles.

1. PROPELLANT PLASMA ACCELERATORS v*SupportedinpartundersupportoftheU.S. Air ForceundercontractF33615-67-C-1395 . ments of satellites.

Cited by 7 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. Discharge Characteristics and System Performance of the Ablative Pulsed Plasma Thruster with Different Structural Parameters;Energies;2022-12-12

2. A characteristic velocity for gas-fed PPT performance scaling;36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit;2000-07-24

3. Ablative Z-pinch pulsed plasma thruster;36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit;2000-07-24

4. Is the gas-fed PPT an electromagnetic accelerator? An investigation using measured performance;35th Joint Propulsion Conference and Exhibit;1999-06-20

5. Pulsed plasma propulsion for a small satellite - Mission COMPASS P3OINT;32nd Joint Propulsion Conference and Exhibit;1996-07-01

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