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NASA NTRS · 19650029851

Solid-propellant rockets.

Lambert, C. H., Jr.

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Abstract

Burning rate, grain geometries and propulsion parameters derived for solid propellant rocket engines

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PROPELLANT GRAIN SPACECRAFT PROPULSION SOLID PROPELLANT ROCKET ENGINE BURNING RATE

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Lambert, C. H., Jr.. 1964-01-01. Solid-propellant rockets.. https://ntrs.nasa.gov/citations/19650029851

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