GAF Pika | |
|---|---|
| Страны | Австралия |
| Роль | Дрон-мишень |
| Первый полет | 28 августа 1952 |
| Построен | 517 |
Teh GAF Jindivik — радиоуправляемый беспилотник-мишень, производимый австралийскими государственными авиационными заводами (GAF). Название происходит от австралийского слова, означающего «преследуемый». Два прототипа с ручным управлением, были построены как GAF Pika (проект в качестве доказательства концепции для тестирования аэродинамики, двигателя и систем радиоуправления, серийный номер A92-1/2, 'B-1/2'. Радиоуправляемый Jindivik первоначально получил обозначение Project B и получил серийные версии серии A93. Пика — австралийское слово, означающее «летун»
Источник: GAF Pika в Википедии
| ГАФ Пика | |
|---|---|
| Фотограф | Владимир Якубов |
| Локализации | Музей RAAF, Пойнт Кук |
| Фотографии | 47 |
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General Characteristics and Role
The GAF Pika was a single-seat, manned, experimental jet aircraft developed by the Government Aircraft Factories (GAF) in Australia. Its primary and sole role was to serve as a proof-of-concept testbed for the larger Jindivik pilotless target drone program. The Pika (an Aboriginal Australian word meaning “flier”) was essentially the Jindivik airframe modified with a cockpit, side air intakes (to clear space for the pilot), and a conventional retractable tricycle undercarriage. Only two prototypes were built (A93-1 and A93-2). By flying the Pika first, engineers could safely test the Jindivik’s unique aerodynamics, the performance of its jet engine, and the complex radio control systems before attempting unmanned flight, making it the only Australian-designed and built manned jet aircraft to date.
| Property | Typical Value (GAF Pika) |
|---|---|
| Тип | Experimental Jet Aircraft / Testbed |
| National Origin | Австралия |
| Производителя | Government Aircraft Factories (GAF) |
| First Flight | October 31, 1951 (or November 4, 1950, sources vary) |
| Экипажа | 1 (Pilot) |
| Max Takeoff Weight | Approx. 1,315 kg (2,900 lb) |
| Длина | 7.08–7.49 m (23 ft 3 in – 24 ft 7 in) |
| Размах крыла | 5.79–5.8 m (19 ft 0 in – 19 ft 0 in) |
Powerplant and Performance
- Engine: 1 x Armstrong Siddeley Adder ASA.1 turbojet engine.
- Thrust: Approx. 3.9 kN (1,050 lbf).
- Maximum Speed: Approx. 756 km/h (470 mph).
- Service Ceiling: Approx. 9,754 m (32,000 ft).
- Endurance: Limited to around 30 minutes due to the reduced fuel load necessitated by the pilot’s cockpit and undercarriage.
- Unique Purpose: The Pika could be flown manually by the pilot or controlled remotely by a ground station, providing crucial training for the future Jindivik operators.
- Air Intakes: Unlike the subsequent Jindivik (which had a dorsal intake), the Pika featured two side-mounted air intakes.
Service History and Legacy
- Test Program: The two prototypes logged over one hundred flights during testing at the Woomera Rocket Range in South Australia.
- Key Findings: The trials confirmed the Jindivik’s aerodynamic stability and performance envelope. One significant result was proving that the final Jindivik design did not require a rudder, leading to cost and weight savings.
- Successor: The knowledge gained from the Pika directly led to the successful development and mass production of the GAF Jindivik, which became a globally exported, high-altitude target drone used by Australia, the UK, Sweden, and the US Navy.
- Final Status: The last flying Pika (A93-2) ended its flying career in 1954. The sole surviving prototype is preserved and on public display at the RAAF Museum in Point Cook, Victoria.
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