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NASA NTRS · 19700057433

Throttleable thruster system design, fabrication and test verification

Abstract

Throttleable thrustor system for Mars soft landing, selecting catalytic decomposition engine from system weight and performance studies

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BibTeXRIS

Kenny, R. J., Reeves, D. F.. 1970-06-01. Throttleable thruster system design, fabrication and test verification. https://ntrs.nasa.gov/citations/19700057433

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