Flat Wing Area
11.1019 m²
Flat Wing Aspect Ratio
8.04
Cruise Speed
185.0746 km/h
Entry Into service
1968-01-01
Maximum Take-Off Weight
0.8732 t (paragliders: kg)
Total Fuel Capacity
109.1062
Maximum Range
708.1114 km
Pictures
No pictures yet for this family.
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 |
Similar airplanes
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