Low-Thrust Solid Rocket Motors for Small, Fast Aircraft Propulsion: Design and Development-Reference-Cited by-同舟云学术

Low-Thrust Solid Rocket Motors for Small, Fast Aircraft Propulsion: Design and Development

Published:2022-01 Issue:1 Volume:38 Page:122-134
ISSN:1533-3876
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Vernacchia Matthew T.¹,Mathesius Kelly J.¹,Hansman R. John¹

Affiliation:

1. Massachusetts Institute of Technology, Cambridge, Massachusetts 02139

Funder

Lincoln Laboratory, Massachusetts Institute of Technology

U.S. Department of Defense

BAE Systems, Inc.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.B38104

Reference30 articles.

1. ShaferJ. I. “Solid-Propellant Motors for High-Incremental-Velocity Low-Acceleration Maneuvers in Space,” Jet Propulsion Lab. JPL-TM-33-528, Pasadena, CA, March 1972, https://ntrs.nasa.gov/search.jsp?R=19720012197.

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