三菱J8M1秀水 | |
|---|---|
| 国 | 日本 |
| 役割 | ロケット式迎撃機 |
| 初飛行 | 1945年7月7日 |
| 構築 | 7 |
ザ 三菱J8M州水 ●ドイツのメッサーシュミットMe 163コメットを基にした日本第二次世界大戦ロケット搭載迎撃機でした。●海軍と陸軍航空サービスの共同プロジェクトとして建造され、J8M(海軍)とKi-200(陸軍)に指定されました。
ソース： 三菱J8M1修水ウィキペディア
| Mitsubishi J8M1 Shusui | |
|---|---|
| カメラマン | 知りません |
| ローカライズ | 知りません |
| 写真 | 33 |
Mitsubishi J8M1 Shusui 01
Mitsubishi J8M1 Shusui 02
Mitsubishi J8M1 Shusui 03
Mitsubishi J8M1 Shusui 04
Mitsubishi J8M1 Shusui 06
Mitsubishi J8M1 Shusui 05
Mitsubishi J8M1 Shusui 07
Mitsubishi J8M1 Shusui 08
Mitsubishi J8M1 Shusui 09
待って、検索三菱J8M1秀水はあなたのために.
関連項目:
| Mitsubishi J8M1 Shusui Walk Around | |
|---|---|
| カメラマン | セス・ヘンドリックス |
| ローカライズ | 知りません |
| 写真 | 21 |
Mitsubishi J8M1 Shusui 01
Mitsubishi J8M1 Shusui 02
Mitsubishi J8M1 Shusui 03
Mitsubishi J8M1 Shusui 04
Mitsubishi J8M1 Shusui 06
Mitsubishi J8M1 Shusui 05
Mitsubishi J8M1 Shusui 07
Mitsubishi J8M1 Shusui 08
Mitsubishi J8M1 Shusui 09
General Characteristics
The Mitsubishi J8M1 Shusui (Autumn Water, or Sharp Sword) was a Japanese World War II interceptor project closely based on the German Messerschmitt Me 163 Komet rocket fighter. It was developed to combat the high-altitude B-29 Superfortress raids. Despite ambitious plans for mass production for both the Navy (J8M) and Army (Ki-200), development was hampered by the loss of German technical data during shipment, and only seven prototypes were built before the war ended. The single powered test flight in July 1945 ended in a crash.
| Property | Typical Value (J8M1 Prototype) |
|---|---|
| 役割 | Rocket-Powered Interceptor |
| メーカー | Mitsubishi Heavy Industries |
| First Powered Flight | July 7, 1945 |
| No. Built | 7 (Prototypes) |
| 乗組員 | 1 (Pilot) |
| 長さ | 6.05 m (19 ft 10 in) |
| 翼 | 9.50 m (31 ft 2 in) |
| Wing Area | 17.73 m² (190.8 sq ft) |
| Loaded Weight | 3,885 kg (8,565 lb) |
Design and Powerplant
- Engine: One Yokosuka Toko Ro.2 (KR10) bi-fuel liquid rocket motor (Japanese license-built version of the Walter HWK 109-509A).
- Thrust: 14.7 kN (1,500 kgp or 3,307 lbf).
- Propellants: Used highly volatile propellants: T-Stoff (oxidizer, hydrogen peroxide) and C-Stoff (fuel, methanol/hydrazine).
- Configuration: Tailless, swept-wing monoplane with fixed skid landing gear (jettisonable wheeled dolly for takeoff).
- Endurance: Due to the high fuel consumption of the rocket engine, powered flight was limited to approximately 5 minutes 30 seconds.
Performance and Armament
- Maximum Speed: Approximately 900 km/h (559 mph, 486 knots) at 10,000 m (32,808 ft).
- Service Ceiling: 12,000 m (39,370 ft).
- Climb Rate: Could reach 10,000 m in roughly 3 minutes 30 seconds.
- Armament (J8M1): Two wing-mounted 30 mm Type 5 cannon (with 53 rounds per gun).
- Armament (Ki-200 Army version): Planned to use two 30 mm Ho-105 cannons or Ho-155 cannons, differing slightly from the Navy variant.
ビュー : 3031
