The SRP is the first Tresnobik aircraft which was built by its founder Jimmy Tresnov for the National Aviation Cup in the year 1942 resulting in second place place.
2 airplanes were built, a prototype and a complete airplane which was destroyed in a fire in the area where it was built, leaving the prototype as an operational model for the race.
Technical data
- Max Speed: 390km/h
- Minimum takeoff speed: 85km/h
- Flight ceilling: 2km
- Recommended flight ceilling: 897m
Activation groups
- AG1:Engine
- AG2:Canopy
- AG3:Parachute
Specifications
General Characteristics
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- Wingspan 32.0ft (9.8m)
- Length 31.4ft (9.6m)
- Height 12.0ft (3.7m)
- Empty Weight 13,913lbs (6,311kg)
- Loaded Weight 14,220lbs (6,450kg)
Performance
- Horse Power/Weight Ratio 0.175
- Wing Loading 7.1lbs/ft2 (34.6kg/m2)
- Wing Area 2,004.8ft2 (186.3m2)
- Drag Points 3250
Parts
- Number of Parts 144
- Control Surfaces 0
- Performance Cost 740
