Rans S-9 Chaos
American homebuilt airplane
From Wikipedia, the free encyclopedia
The Rans S-9 Chaos is an American single-engined, tractor configuration, single-seat, mid-wing monoplane designed by Randy Schlitter for aerobatics and manufactured by Rans Inc. The Chaos is available in kit form for amateur construction.[1][2][3][4][5][6][7]
| S-9 Chaos | |
|---|---|
| General information | |
| Type | Kit aircraft |
| National origin | United States |
| Manufacturer | Rans Inc |
| Designer | Randy Schlitter |
| Status | In production |
| Number built | 215 (2011) |
| History | |
| Manufactured | 1986-2006, 2009-present |
| Introduction date | 1986 |
| First flight | 1986 |
| Variant | Rans S-10 Sakota |
Production of the S-9 was ended as part of Rans' reorganization of its product line on 1 June 2006, after having been available for 20 years, but the S-9 was reintroduced in about 2009 and is again available.[3][8][9]
Design and development
The S-9 Chaos was designed by Randy Schlitter in 1986 as an inexpensive aerobatic aircraft that will allow sportsman competition aerobatics to be flown or even advanced aerobatics if inverted fuel and oil systems are installed. The Chaos is also a capable cross country aircraft.[3]
Like many Rans models, the S-9 features a welded 4130 steel tube cockpit, with a bolted aluminum tube rear fuselage. All fuselage, wing and tail surfaces are covered in dope and fabric. The reported construction time is 500 man-hours.[1][2]
The Chaos has conventional landing gear. The basic engine is the Rotax 503 of 50 hp (37 kW), with the Rotax 582 of 64 hp (48 kW) and the Hirth 3701 of 100 hp (75 kW) available as options.[1][2][10]
The S-10 Sakota aerobatic two-seater was later developed from the S-9.[2]
Operational history
Specifications (S-9)
Data from Kitplanes and Aerocrafter[1][2]
General characteristics
- Crew: One
- Length: 15 ft 8 in (4.78 m)
- Wingspan: 22 ft 0 in (6.71 m)
- Wing area: 91.5 sq ft (8.50 m2)
- Empty weight: 320 lb (145 kg)
- Gross weight: 670 lb (304 kg)
- Fuel capacity: 9 US gallons (34 litres)
- Powerplant: 1 × Rotax 503 , 50 hp (37 kW)
- Propellers: 2-bladed wooden
Performance
- Cruise speed: 85 mph (137 km/h, 74 kn)
- Stall speed: 33 mph (53 km/h, 29 kn)
- Range: 210 mi (340 km, 180 nmi)
- Service ceiling: 15,500 ft (4,700 m)
- Rate of climb: 800 ft/min (4.1 m/s)
Avionics
- none