ROCKET, FLARE, 2.75-INCH W/M257 ILLUMINATING WARHEAD
No Image Available Filler and Weight
NA,
Body and Overall Weight
Aluminum, 21.8 lb
Color
Olive drab w/white markings
Type of Round, DODIC
MK40, Mod 3 MK66 Mod 1, 2. and 3, 1340 -H180
Description:
This flare rocket is an air-to-ground rocket primarily deployed from rotary-wing and other low-speed aircraft. It is employed with the lowspin folding-fin MK40 motor and with the spin stabilized wrap around fin MK66 motor Mods 1,2, and 3. The M257 illuminating warhead consists of an ignition system, flare, main parachute, drogue parachute assembly and an integral fuze and delay assembly. The warhead is enclosed in an aluminum case. The setback-actuated fixed time integral fuze provides a standoff’ distance of approximately 3,000 meters. The arming fuze and delay assembly is actuated by motor acceleration.
Use:
To provide helicopters with target illuminating capability from a safe standoff distance in a hostile environment.
Functioning:
The rocket with warhead, flare, M257, is fired from helicopter with standard 2.75-in. motor MK40 or MK66 to attain elevation between 2000 and 4000 ft at 3000 m downrange, Upon rocket launch, the M442 fuze arms upon acceleration (17 G’s approximately required ). After 1.5 seconds (at motor burnout), the fuze functions initiating delay train, After nine seconds, delay ignites first expulsion charge in fuze assembly. Gas pressure forces pusher plate forward, shears pin. separates motor and adapter section from remainder of warhead. Rocket velocity is now 800 fps approximately. The deflector plate, attached by cable to motor adapter, is extended into airstream, deflects path of motor and adapter. Pusher plate, attached to drogue chute, deploys drogue, Rocket warhead velocity then decreases to 200 fps, approximately, during the next two seconds. Upon deployment of drogue chute, the gas generator is activated by pull on lanyard attached to drogue. After two seconds, tile gas generator functions the second expulsion charge located in retainer block of drogue housing. Gas pressure forces pusher plate forward, shearing pins and separating drogue housing from main chute insert and candle assembly, The pusher plate is attached by a threadline to the pilot chute. The pilot chute is deployed, and, in turn, pulls bag off main chute. The main chute now deploys the steel cable which is attached to the main chute shroud lines on one end, and, in turn, pulls a lanyard attached to candle igniter assembly. The pull on the lanyard rotates a bellcrank, releasing the firing pin. The firing pin fires a rifle primer, which fires boron pellets. The boron pellets ignite a propellant wafer. Propellant ignites the candle. Ignition gases pressurize nose cap, blowing it free. The candle, suspended from the main chute, is now burning. During the first 15 seconds, the igniter housing is burned away, The candle descends at 15 fps, burns for 100 seconds with a minimum light output of one million candle power (CP).
Munition Components:
  • Fuze: Model M434, Type Base detonating
  • Propellant M7
  • Fuze: Model M434, Type Base detonating
  • Propellant M7
  • Fuze: Model M434, Type Base detonating
  • Propellant M7
Data Source:
TM 43-0001-30 Dec 1981
Munitions Tech Data Sheet:
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