Reduced temperature sensitivity launch motor

Fluid sprinkling – spraying – and diffusing – Reaction motor discharge nozzle – With erodible – frangible or fusible nozzle part

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Details

60233, 60238, F02K 106

Patent

active

H00007951

ABSTRACT:
A rocket motor that has a main exhaust nozzle area and a secondary exhaust ozzle area with the secondary exhaust nozzle area being closed by burst discs that rupture and open secondary nozzle areas when predetermined temperatures and pressures are reached when propellant is burned inside the rocket motor.

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