Leduc 0.10 uur | |
|---|---|
| Land | Frankrijk |
| Role | Onderzoeksvliegtuigen |
| Eerste vlucht | van 21 oktober 1947 |
| Gebouwd | 3 |
De Leduc 0.10 uur was een onderzoeksvliegtuig gebouwd in Frankrijk, een van 's werelds eerste vliegtuigen die uitsluitend werd aangedreven door een ramjet
Bron: Leduc 0.10 op Wikipedia
| Leduc 010 Walk Around | |
|---|---|
| Fotograaf | Unknow |
| Lokalisatie | Onbewust |
| Foto 's | 11 |
Zie ook:
General Characteristics
The Leduc 0.10 was a groundbreaking French experimental aircraft designed by René Leduc and built by Breguet Aviation. It is famous for being one of the world’s first aircraft to fly powered solely by a ramjet engine. Designed starting in 1938 and finally completed after World War II, the aircraft was built purely to test the viability of ramjet propulsion. Its unique fuselage featured a double-walled cylindrical design, where the pilot sat in a cockpit within the inner shell, and the annular space between the inner and outer shells served as the air inlet for the ramjet. Only two prototypes were initially built.
| Property | Typical Value (Leduc 0.10) |
|---|---|
| Role | Experimental Research Aircraft |
| National Origin | Frankrijk |
| Fabrikant | Breguet Aviation (Designed by René Leduc) |
| First Flight (Powered) | April 21, 1949 |
| Bemanning | 1 (Pilot) or 2 (Pilot/Observer) |
| Lengte | 10.25 m (33 ft 7 in) |
| Spanwijdte | 10.52 m (34 ft 6 in) |
| Max Takeoff Weight | 2,800 kg (6,173 lb) |
| Constructie | All-metal structure with conical mid-wings |
Powerplant and Performance
- Engine: 1 x Leduc ramjet (Leduc Tuyère 5 viroles).
- Thrust: ~15.7 kN (3,520 lbf) at full power (ramjets only produce thrust above a minimum forward speed).
- Propulsion Method: The ramjet has no moving parts (like a turbine) and relies on the aircraft’s high speed to compress incoming air (ram compression) before mixing with fuel and igniting it.
- Takeoff: Could not take off unassisted; it was a parasite aircraft carried aloft by a mother ship (usually a Sud-Est SE.161 Languedoc four-engined airliner) and released at speed and altitude.
- Maximum Speed: Achieved 960 km/h (597 mph, Mach 0.85) in tests.
- Service Ceiling: 12,000 m (39,400 ft).
- Rate of Climb: Achieved 40 m/s (7,900 ft/min), exceeding the best jet fighters of the time.
Design and Legacy
- Pilot Safety: The nose section containing the cockpit was designed to be jettisonable in an emergency, allowing the pilot to escape with a parachute.
- Visibility: The pilot’s forward view was via a Perspex cone (Plexiglas) at the nose, with side vision provided by small portholes on the outer shell.
- Significance: The Leduc 0.10 proved the viability of the ramjet as an aviation powerplant, paving the way for further French ramjet experiments, including the Leduc 0.21 and the partially successful Leduc 0.22 supersonic interceptor prototype.
- Preservation: The third aircraft built, initially designated 0.11 or 0.16, is now preserved at the Musée de l’Air et de l’Espace at Le Bourget, France.
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