Beagle Pup

Length
7.0104 m
Flat Wing Span
9.4488 m
Height
2.1336 m
Flat Wing Area
11.1019 m²
Flat Wing Aspect Ratio
8.04
Max Seating
2
Cruise Speed
185.0746 km/h
Max Speed
222.0895 km/h
Max Ceiling
4480.56 m
Number of Engines
1
Aircraft Engine
First Flight
1967-04-08
Entry Into service
1968-01-01
Number Built
175
Maximum Take-Off Weight
0.8732 t (paragliders: kg)
Total Fuel Capacity
109.1062
Maximum Range
708.1114 km

Pictures

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Aircraft Weight Variants

Aircraft Maximum Take-Off Weight (t (paragliders: kg)) Total Fuel Capacity Maximum Range (km)
Beagle Pup 0.8732 109.1062 708.1114

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Airspeed Queen Wasp 7.0104 9.4488 Compare
Bird Wing Imperial Curtiss OX-5 7.0104 9.4488 2 Compare
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All data (28 fields)
Name
Beagle Pup
Manufacturer
Beagle Aircraft
Description
The Beagle B.121 Pup is a 1960s British 2–4 seat single-engined training and touring aircraft built by Beagle Aircraft Limited at Shoreham Airport and Rearsby Aerodrome.
ICAO Code
PUP
First Flight
1967-04-08
Entry Into service
1968-01-01
Production End
1970-01-01
Designer
Beagle Aircraft
Type
General Aviation
Length (m)
7.0104
Height (m)
2.1336
Cockpit Crew
1
Max Seating
2
Max Speed (km/h)
222.0895
Cruise Speed (km/h)
185.0746
Min Speed (km/h)
90.1233
Max Ceiling (m)
4480.56
Rate of Climb (m/s)
4.064
Capacity Description
2 passengers
Number Built
175
Powerplant Description
1 × Lycoming O-320-A2B air-cooled flat-four, 112 kW (150 hp) each
Wikipedia Article (URL)
en.wikipedia.org/wiki/Beagle_Pup
Flat Wing Span (m)
9.4488
Flat Wing Area (m²)
11.1019
Flat Wing Aspect Ratio
8.04
Wake Category
L
Aircraft Engine
Lycoming O-320
Number of Engines
1