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Massachusetts Institute of Technology

A performance study of a pulsed solid fuel microthruster.

Abstract

dc:description

Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Thesis. 1969. M.S.

Degree

thesis:*
Department dc:contributor.department
Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics
Grantor dc:publisher
Massachusetts Institute of Technology
Year dc:date.issued
1969

Author and committee

dc:creator, dc:contributor.*
Author dc:creator
  • Radley, Roger James
Advisor dc:contributor.advisor
  • Albert Solbes.

Subjects

dc:subject × 1

Rights

dc:rights
Statement dc:rights
  • M.I.T. theses are protected by copyright. They may be viewed from this source for any purpose, but reproduction or distribution in any format is prohibited without written permission. See provided URL for inquiries about permission.
Language dc:language.iso
eng

Identifiers

dc:identifier.*
Handle dc:identifier.uri
http://hdl.handle.net/1721.1/13544
OAI identifier oai:identifier
oai:dspace.mit.edu:1721.1/13544

Chain of custody

source
Harvested from
MIT
Base URL
dspace.mit.edu/oai/request
Last updated
2026-07-22
Source record
OAI-PMH GetRecord
citation

Radley, Roger James. A performance study of a pulsed solid fuel microthruster.. Massachusetts Institute of Technology, 1969. http://hdl.handle.net/1721.1/13544