FG-86 Solid Rocket Motor
SKU: MD-P00592·Spare Parts & Components·受注生産
概要
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
技術仕様
Specifications. 主な仕様： 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。
技術仕様 — 1 groups
主な仕様： 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。
技術仕様
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
対応機体
この部品は以下のプラットフォームに対応します。
適合データの準備中です。機体の型番をお知らせください。