FG-86 Solid Rocket Motor
SKU: MD-P00592·Spare Parts & Components·Made to Order
Overview
FG-86 solid rocket motor is a conventional solid rocket motor developed by Beijing Institute of Power Machinery. It consists of front head, combustion chamber, nozzle and igniter. The engine adopts head ignition technology. After ignition, the charge continues to burn and generate rated thrust, and then the aircraft falls off freely under the action of aerodynamic force and gravity when it reaches the specified speed. It can be used as the first stage take-off power device of UAV and missile Main Performance Index of FG-86 solid rocket motor Operating Temperature：-40℃～+55℃ Operational Height：0km～10km
Technical specification
Specifications. Key specifications: Code Name FG-86, Diameter 220mm, Length 1421mm, Weight 80kg, Total Impulse 120KN s, Thrust 25KN56KN, Working Time 4s, Operating Temperature -40℃～+55℃, Operational Height 0km～10km.
Technical specification — 1 groups
Key specifications: Code Name FG-86, Diameter 220mm, Length 1421mm, Weight 80kg, Total Impulse 120KN s, Thrust 25KN56KN, Working Time 4s, Operating Temperature -40℃～+55℃, Operational Height 0km～10km.
Technical specifications
Specifications
- Code Name
- FG-86
- Diameter
- 220mm
- Length
- 1421mm
- Weight
- 80kg
- Total Impulse
- 120KN s
- Thrust
- 25KN56KN
- Working Time
- 4s
- Operating Temperature
- -40℃～+55℃
- Operational Height
- 0km～10km
Compatible aircraft
This part fits the following platforms.
Fitment data pending — contact us with your aircraft model.