Burning rate modifiers for solid propellants

Explosive and thermic compositions or charges – Structure or arrangement of component or product – Solid particles dispersed in solid solution or matrix

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

149 194, 149 20, C06B 4510

Patent

active

040000249

ABSTRACT:
A solid propellant formulation which utilizes the addition of low levels of transition metal fluorides, such as cupric fluoride and ferric fluoride, as a modifying agent to increase the propellant burning rate while simultaneously decreasing its pressure exponent.

REFERENCES:
patent: 3476622 (1969-11-01), Harada et al.
patent: 3752703 (1973-08-01), Toy et al.
patent: 3753811 (1973-08-01), Julian et al.
patent: 3801385 (1974-04-01), Mastrolia et al.
patent: 3876477 (1975-04-01), Eldridge et al.
patent: 3932240 (1976-01-01), Braun et al.

LandOfFree

Say what you really think

Search LandOfFree.com for the USA inventors and patents. Rate them and share your experience with other people.

Rating

Burning rate modifiers for solid propellants does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Burning rate modifiers for solid propellants, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Burning rate modifiers for solid propellants will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-147165

  Search
All data on this website is collected from public sources. Our data reflects the most accurate information available at the time of publication.