Dual combustion missile system

Details Dual combustion missile system Dual combustion missile system

1975-09-03

1977-03-22

Brown, David H.

Ordnance

Recoilless gun

Having a reaction mass

89 1816, F41F 302, F41F 1500

Patent

active

040129870

ABSTRACT:
A missile system with an ogival projectile for operation in a trajectory m a tubular launch tube includes a housing and a slug respectively slidable in the projectile and the housing with the projectile and housing respectively including combustion chambers and pistons enclosing propellant grains therein. The projectile and slug are respectively launched forwardly in the trajectory and rearwardly and the housing is ejected from the projectile responsive to simultaneous ignition of the propellant grains. The piston is ejected from the projectile responsive to continued ignition of the corresponding propellant grain.

REFERENCES:
patent: 1395630 (1921-11-01), Davis
patent: 3771417 (1973-11-01), Schnabele et al.
patent: 3800656 (1974-04-01), Schnabele
patent: 3815469 (1974-06-01), Schubert et al.

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