V-1 flying bomb | |
|---|---|
| 국가 | 나치 독일 |
| 역할 | 순항 미사일 |
| 서비스 중 | 1944–1945 |
| 내장 | Unknow |
Tthe V-1 비행 폭탄 (독일어: Vergeltungswaffe 1 "Vengeance Weapon 1)"은 연합군에게는 버즈 폭탄 또는 낙서벌레로, 독일에서는 Kirschkern(체리 스톤) 또는 Maikäfer(메이버그)로도 알려져 있으며, 공식 RLM 항공기 명칭인 Fi 103은 초기 순항 미사일이자 동력을 위해 펄스제트를 사용하는 유일한 생산 항공기였습니다.
소스: 위키 백과에 V-1 비행 폭탄
| Fieseler Fi 103 V-1 ‘Buzz Bomb’ Walk Around | |
|---|---|
| 사진 작가 | 마이클 베놀킨 |
| 로컬라이제이션 | Unknow |
| 사진 | 41 |
| Fieseler Fi 103 V1 Rreichenberg gerat Walk Around | |
|---|---|
| 사진 작가 | Unknow |
| 로컬라이제이션 | Unknow |
| 사진 | 14 |
참고 항목:
General Characteristics and Role
The Fieseler Fi 103, better known by the Nazi propaganda name Vergeltungswaffe Eins (“Vengeance Weapon 1”) or V-1, was the world’s first operational cruise missile. Developed by Germany during World War II, it was a pilotless aircraft powered by a simple pulsejet engine, which produced a distinctive loud, sputtering sound that earned it the nickname “Buzz Bomb” or “Doodlebug” from the British. The V-1’s primary purpose was to be launched against large target areas, particularly London and later Antwerp, as a terror weapon in response to Allied bombing raids on Germany. Though highly inaccurate, its deployment marked a significant step in missile technology.
| Property | Typical Value |
|---|---|
| 역할 | Unmanned Surface-to-Surface Cruise Missile / Terror Weapon |
| National Origin | 나치 독일 |
| 제조업체 | Gerhard Fieseler Werke |
| Service Entry | 13 June 1944 |
| 승무원 | 0 (Unmanned) |
| Launch Weight | Approx. 2,150–2,250 kg (4,740–4,960 lb) |
| 길이 | 7.7–8.32 m (25 ft 3 in – 27 ft 3 in) |
| 윙스 팬 | 5.37 m (17 ft 7 in) |
| Production Total | Approx. 30,000 built |
Powerplant and Performance
- Engine: One Argus As 109-014 Pulsejet impulse duct engine.
- Thrust: Approx. 300 kgf (660 lbf).
- Fuel: Gasoline (propelled by compressed air rather than a fuel pump).
- Maximum Speed: 640–650 km/h (400–405 mph).
- Note: This relatively low speed allowed it to be intercepted by fast fighter aircraft like the Hawker Tempest and Spitfire.
- Operational Range: Approx. 240–330 km (150–205 mi).
- Service Ceiling: Approx. 600–900 m (2,000–3,000 ft).
- Launch Method: Primarily launched from inclined ground-based ramps using a steam catapult (Walter Catapult), or air-launched from Heinkel He 111 bombers.
Guidance and Warhead
- Guidance System: Simple gyrocompass-based autopilot (Askania) for directional stability and a pre-set air log/propeller counter.
- Targeting Mechanism: Distance was controlled by a small nose-mounted propeller which, after a set number of rotations, would trigger a mechanism to cut the fuel supply and cause the missile to dive onto its target.
- Warhead: High-explosive Amatol 39 or Trialen.
- Warhead Weight: Approx. 850 kg (1,870 lb).
- Inaccuracy: The crude guidance system meant the V-1 was inaccurate, limiting its use to large population centers.
- Variant: The Fieseler Fi 103R Reichenberg was a late-war manned version intended for suicide missions, though never operationally deployed.
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