Ambrosini Sagittario
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| Sagittario | |
|---|---|
| Type | Research aircraft |
| Manufacturer | Ambrosini |
| Maiden flight | 1953 |
| Number built | 1 |
The Ambrosini Sagittario was an Italian aerodynamic research aircraft based on the manufacturer's S.7. New swept wings and tail surfaces of wooden construction were fitted to the S.7 fuselage. The wing leading edge was swept at 45 degrees. At first, the S.7's piston engine was retained and the aircraft was known as the Freccia (Arrow). After several test flights in this configuration (the first on 5 January 1953), the piston engine was removed and replaced with a Turboméca Marboré turbojet of 3.7 kN (840 lbf) thrust, and the aircraft renamed the Sagittario. The engine air inlet was in the extreme nose, and the exhaust was routed out the bottom of the fuselage, under the cockpit. The tail wheel undercarriage was retained, so special shielding was added to protect the tail wheel from the engine exhaust.
[edit] Specifications
General characteristics
- Crew: one pilot
- Powerplant: 1 × Turboméca Marboré turbojet, 3.7 kN (840 lbf) thrust
Performance
- Maximum speed: 560 km/h (350 mph)
[edit] References
- Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions, 57.
- Flight, 24 April, 1953, pp. 508-509
[edit] See also
Related development Ambrosini S.7 - Aerfer Sagittario 2 - Aerfer Leone
Comparable aircraft Yakovlev Yak-15
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