Firefox Special Ammunition Engine Series
SKU: MD-P00447·Spare Parts & Components·Made to Order
Overview
It is used in military and civil fields such as small-caliber light missiles, extended-range guided projectiles and fire-extinguishing bombs, including projectile extended-range engines, bottom row devices, small-caliber intelligent ammunition engines and fire-extinguishing bomb boosters. This series of products has a variety of models, with a diameter ranging from 40mm to 150mm, and a total impact range from 1.5kN s to 40kN s. Technical characteristics Adopting the high-overload resistance design of the shell and charge, the miniaturized and refined design of the charge combustion chamber and the nozzle, and the optimized design of the insulation layer, it solves the problem of safety and reliability under high overload, small thrust, long-term working environment, etc. Pain points of use. Average thrust: 8kN/0.9kN/0.24kN Working time: 0.045s/1s/15s Application scenario A missile launching engine and a single-chamber double-propelling active engine Application scenario: a special guided missile:
Technical specification
Specifications. Key specifications: Average thrust 8kN/0.9kN/0.24kN, Working time 0.045s/1s/15s, Total length 615mm, Diameter 80mm, Total impulse 4.86kN s, Total weight 4.5kg, Application scenario a special guided missile:.
Technical specification — 1 groups
Key specifications: Average thrust 8kN/0.9kN/0.24kN, Working time 0.045s/1s/15s, Total length 615mm, Diameter 80mm, Total impulse 4.86kN s, Total weight 4.5kg, Application scenario a special guided missile:.
Technical specifications
Specifications
- Average thrust
- 8kN/0.9kN/0.24kN
- Working time
- 0.045s/1s/15s
- Total length
- 615mm
- Diameter
- 80mm
- Total impulse
- 4.86kN s
- Total weight
- 4.5kg
- Application scenario
- a special guided missile:
Compatible aircraft
This part fits the following platforms.
Fitment data pending — contact us with your aircraft model.