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Patent

Solid propellant burning rate detector

About
The article was published on 1962-12-14. It has received 16 citations till now. The article focuses on the topics: Burn rate (chemistry) & Propellant.

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Citations
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Patent

Test apparatus for combustion evaluation

TL;DR: A combustion chamber for testing under actual burning conditions the ability of air augmented solid propellants to meet operational requirements under subsonic or supersonic environments is presented in this paper.
Patent

Rocket burn rate testing device

TL;DR: In this paper, a closed chamber designed to hold one or more strands of a solid propellant is equipped with igniting means, pressure indicating means, and burning rate indicating means.
Patent

Apparatus and method for measuring instantaneous burning rate of solid propellant

TL;DR: In this paper, an apparatus and method for measuring the instantaneous burning rate of solid propellant is presented, which consists of a sealed combustor, the combustor is internally provided with a weighing apparatus for placing a propellant sample to be measured, and the weighing apparatus is connected to a data acquisition system in data connection.
Patent

Solid propellant powered rocket motor control system

TL;DR: In this paper, a control system for a solid propellant powered rocket motor utilizing an electrical impulse generating sensor means responsive to heat generated by the burning propellant is presented. But the system is not suitable for the use in a satellite.
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