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A COMPOSITION OF A PROPELLANT FOR SPONTANEOUS THRUST TERMINATION IN A ROCKET.

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A COMPOSITION OF A PROPELLANT FOR SPONTANEOUS THRUST TERMINATION IN A ROCKET.

ORDINARY APPLICATION

Published

date

Filed on 31 August 2020

Patent Information

Application ID202031037390
Date of Application31/08/2020

Documents

NameDate
202031037390-COMPLETE SPECIFICATION [31-08-2021(online)].pdf31/08/2021
202031037390-DRAWING [31-08-2021(online)].pdf31/08/2021
202031037390-FORM 1 [31-08-2020(online)].pdf31/08/2020
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