When the engine one is Wasp Jr. T1B2, what the number needed for takeoff power one?
Engine Power, continuous Critical altitude This is the highest altitude at which the engine can achieve its full continuous power rating. Above this altitude, power falls off with height as with a naturally aspirated engine . See Supercharger#Altitude effects for details. Power, takeoff Compression ratio Supercharger gear ratio Octane rating Dry weight
Pratt & Whitney R-985 Wasp Junior
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1-1123802-1
Specifications (R-985 Wasp Junior SB)
Specifications for different R-985 Wasp Junior variants
Wasp Jr. A hp (kW) at 2,000 RPM sea level same 5.0:1 7:1 68 lb (kg)
Wasp Jr. TB hp (kW) at 2,200 RPM sea level hp (kW) at 2,300 RPM 6.0:1 8:1 80 lb (kg)
Wasp Jr. SB hp (kW) at 2,200 RPM ft (m) hp (kW) at 2,300 RPM 6.0:1 10:1 80/87 lb (kg)
Wasp Jr. T1B2 hp (kW) at 2,300 RPM ft (m) same 6.0:1 10:1 80/87 lb (kg)
Wasp Jr. B4 hp (kW) at 2,300 RPM ft (m) same 6.0:1 10:1 80/87 lb (kg)
table_1123802_1
SELECT COUNT Power, takeoff FROM table WHERE Engine = Wasp Jr. T1B2
Wasp Jr. T1B2