Engineering:Kingsford Smith Cropmaster
| Kingsford Smith KS-3 Cropmaster | |
|---|---|
| |
| KS-3 Cropmaster | |
| Role | agricultural aircraft |
| Manufacturer | Kingsford Smith Aviation Services Pty. Ltd. |
| Designer | C. W. (Bill) Smith |
| First flight | 1957 |
| Developed from | CAC Wackett |
The KS-3 Cropmaster was an Australian agricultural aircraft developed from the CAC Wackett, an aircraft used for training purposes during World War II.
Design and development
The KS-3 was developed from the CAC Wackett by Kingsford Smith Aviation Services Pty. Ltd. (KSAS) for aerial top-dressing and spraying.
John Brown OBE had purchased KSAS in 1946 (the company was started by Sir Charles Kingsford Smith in 1933, but was defunct at the time of Brown's purchase) and made several attempts to develop an agricultural aircraft suitable for Australian conditions. Modifications to a war-surplus CAC Wackett airframe (C/N 283, VH-AJH) had resulted in the KS-1 and KS-2, but feedback from Bill Boulden (Chief Pilot at Airwork Pty Ltd in Perth) indicated the hopper should be placed behind the pilot, for better visibility, easier loading of the hopper and avoiding cleaning the windscreen after loading. KSAS converted Wackett C/N 299 to become the first KS-3 Cropmaster, and it had its first flight on 29 November 1957.
All KS-3 airframes were converted from war-surplus Wackett airframes. The changes included reducing the wing and tail-plane incidence, covering the fixed leading-edge slots, removing the rounded wing-tip fairings, adding a 13 cubic foot (400 litre) aluminium chemical hopper in place of the rear seat and modifying the control routes around the hopper outlet.
Specifications (Kingsford Smith Aviation Services KS-3 Cropmaster)
General characteristics
- Crew: 1
- Length: 26 ft (7.9 m)
- Wingspan: 37 ft (11 m)
- Height: 7 ft 11 in (2.41 m)
- Wing area: 184 sq ft (17.1 m2)
- Airfoil: root: NACA 2216; tip: NACA 2209[1]
- Gross weight: 2,620 lb (1,188 kg)
- Powerplant: 1 × Warner Super Scarab 7-cylinder air-cooled radial piston engine, 175 hp (130 kW)
- Propellers: 2-bladed fixed-pitch propeller
Performance
- Cruise speed: 97 mph (156 km/h, 84 kn)
- Wing loading: 14.2 lb/sq ft (69 kg/m2)
See also
References
- ↑ Lednicer, David. "The Incomplete Guide to Airfoil Usage". https://m-selig.ae.illinois.edu/ads/aircraft.html. Retrieved 16 April 2019.
- Tiger Moth, CT-4, Wackett & Winjeel in Australian Service Stewart Wilson. Aerospace Publications Pty. Ltd. ISBN:1-875671-16-1
- Aerial Agriculture in Australia Derrick Rolland. 1996 Aerial Agricultural Association of Australia Ltd. ISBN:0-646-24840-5
- original company documents and plans held by Fred Burke
- research material compiled by Allyn Eckford
- photographs by Ben Danneker
External links
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