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STUDY OF MONOPROPELLANTS FOR ELECTROTHERMAL THRUSTERS DESIGN AND FABRICATION TASK SUMMARY REPORT

机译：用于电热推力器设计和制造任务的单板的研究总结报告

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The objective of the “Study of Monopropellants for Electrothermal Thrusters” program is to determine the feasibility of operating small trust level ellectrotnermal thrusters with monopropellants other than MIL-grade hydrazine. The work scope includes analytical wherein monopropellants with freezing points lower than MIL-grade hydrazine are evaluated spacecraft attitude control.

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作者
J.D. Kuenzly;
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作者单位

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年度 1974
页码 1-29
总页数 29
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Monopropellant - Electrothermal - Thruster - Hydrazine Substitutes;

机译：单组元推进剂 - 电热 - 推进剂 - 肼替代品;

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STUDY OF MONOPROPELLANTS FOR ELECTROTHERMAL THRUSTERS DESIGN AND FABRICATION TASK SUMMARY REPORT

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