Gas propellor for guided missile

Details Gas propellor for guided missile Gas propellor for guided missile

F - Mech Eng,Light,Heat,Weapons

02

K

102/5

F02K 9/90 (2006.01) F02K 9/80 (2006.01)

Patent

CA 1244280

ABSTRACT OF THE DISCLOSURE Gas propellor having at least one pair of diametrically opposed lateral nozzles in order to supply a thrust force directed towards the rear of the missile or projectile and comprising a cake of solid propellant relatively insensitive to the combustion pressure, and opening-closing valves of each of the nozzles, these valves being sliding elements provided with pneumatic flip-flop actuators that are controlled by control circuits including a logic operator allowing to prevent the situation or state of the valves corresponding to the simultaneous closing of the two nozzles of a same pair, and the sliding elements of the valves being provided with mechanical safety means in order to limit the relative displacement of these sliding elements.

471557

Affiliated with

Also associated with

Rating

Gas propellor for guided missile does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Gas propellor for guided missile, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Gas propellor for guided missile will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFCA-PAI-O-1211507