Smith XP-99 Prop-Jet
| XP-99 Prop-Jet | |
|---|---|
| Role | Six seat business aircraft |
| National origin | United States |
| Manufacturer | Mike Smith Aero Inc |
| Designer | Mike Smith |
| First flight | 29 July 1982 |
| Number built | 1 |
|
| |
The Smith X-99 Prop-Jet was a six seat turboprop powered business aircraft designed in the United States in the 1980s. Only one was built.
Design and development
The Prop-Jet was an attempt to produce a small, propeller driven business aircraft capable of cruising at speeds above 350 mph (560 km/h). It was powered by a 550 shp (410 kW) Pratt & Whitney Canada PT6 turboprop engine, mounted in a long nose and driving a four blade, constant speed propeller. The fuselage was a monocoque constructed from graphite and glass-fibre epoxy sandwich. The pressurised cabin accommodated pilot and five passengers in three rows of seats, with a baggage space behind. Access was by port side doors forward and another over the trailing edge on the other side. The tail unit was made from Kevlar/graphite/glass fibre epoxy sandwich. The fin was swept and the tailplane mounted, with anhedral, almost at the top of it. The elevator carried an electrically driven trim tab.[1]
To speed the completion of the first prototype, the Prop-Jet used the wing and undercarriage of a Beechcraft Baron 58P, though a composite structure wing was envisaged for production aircraft. The Beech wing was a two spar aluminium box structure, without sweep and mounted between mid and low positions with dihedral of 6° and fitted with slotted Fowler flaps. The tricycle undercarriage was enclosed behind doors after retraction.[1]
The Prop-Jet flew for the first time on 29 July 1982. By 1985 Mike Smith was reported as seeking financial backers[1] but only the one prototype Prop-Jet was built.[2]
Specifications
Data from Jane's All the World's Aircraft 1985–86[1] All performance figures at maximum take-off weight except where noted.
General characteristics
- Crew: One
- Capacity: Five passengers
- Length: 30 ft 7 in (9.32 m)
- Wingspan: 37 ft 10 in (11.53 m)
- Height: 10 ft 6 in (3.2 m)
- Wing area: 119.0 sq ft (11.06 m2)
- Aspect ratio: 12.02
- Airfoil: modified NACA 23016.5 at root, 23012 at tip
- Empty weight: 3,153 lb (1,430 kg)
- Max takeoff weight: 6,000 lb (2,722 kg)
- Fuel capacity: 220 US gal (832.5 L; 183 Imp gal)
- Powerplant: 1 × Pratt & Whitney Canada PT6A-41 turboprop, 550 hp (410 kW) derated from 634 kW (850 hp)
- Propellers: 4-bladed Hartzell Propeller Type HC-B4TN-3AL/LT1073F-12-5, 7 ft 6 in (2.29 m) diameter constant speed
Performance
- Cruising speed: 325 mph; 282 kn (523 km/h) economical, at 31,000 ft (9,450 m)
- Stall speed: 86 mph; 75 kn (138 km/h) flaps down,power off
- Range: 1,448 mi (1,258 nmi; 2,330 km) with maximum payload
- Ferry range: 1,544 mi (1,342 nmi; 2,485 km) with maximum fuel
- Service ceiling: 31,000 ft (9,449 m) service
- Rate of climb: 3,500 ft/min (17.8 m/s) at sea level at weight of 5,182 lb (2,350 kg)
- Wing loading: 50.0 lb/sq ft (244.1 kg/m2)
- Power/mass: 0.093 shp/lb (0.150 kW/kg)
- Take-off distance to clear 50 ft (15 m): 2,376 ft (724 m)
- Landing distance from 50 ft (15 m): 2,498 ft (761 m)
Avionics
- Collins nav/com, ADF, transponder
- Texas Instruments TI-9100C LORAN
- Full blind flying instrumentation
