METHOD FOR ELECTRICALLY INITIATING AND CONTROLLING THE BURNING OF A PROPELLANT CHARGE AND PROPELLANT CHARGE
Assignee
FORSVARETS FORSKNINGSANSTALT
Filed
Jun 7, 1995
Granted
Dec 29, 1998
Location
VASTERHANINGE SE
Abstract
The invention relates to a propellant charge comprising a compact propellant and a method for electrically initiating and controlling the burning of such a propellant charge. Electrothermal energy is supplied to the propellant charge by feeding electric current over electrically conductive surfaces (6, 7, 19) in the propellant, and that said supply is made to different parts or zones (15) of the propellant charge at different points of time during the burning. The invention specifically relates to a projectile propellant charge having a first end (9) facing the projectile (4) and a second end (10) facing the back (3) of the weapon. The electrothermal energy is then supplied to the propellant charge, beginning in the first end thereof and then successively to the second end thereof by feeding the current at each point of time over an axially restricted part (15) of the propellant charge.
Source: Google Patents
35 USC §181 Secrecy Order
Imposed
Jan 30, 1997
Rescinded
Feb 12, 1998
Duration
1 year
Inventor
- 1HENRIK ALMSTROM
Record Details
- Patent number
- US 5854439
- Application
- 08460011
- Aerospace match
- Yes
- Dataset source
- 35 USC §181 SO records
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