|
|
|
the Beagle Pup 100
Specifications
Pup-100 (B.121 Series 1)
Fully
aerobatic light aircraft with
accommodation for two adults. Powered
by 100 hp Rolls-Royce/Continental
0-200-A four cylinder engine, driving
a McCauley type 1A105/SCM 7053 two
blade fixed-pitch metal p ropeller,
diameter 1.78m. Fuel capacity 24 Imp.
gallons (109 litres).
|
Dimensions, External |
|
Wing span |
31ft 0in |
(9.45m) |
|
Length overall |
22ft 11in |
(6.99m) |
|
Height overall |
7ft
6in |
(2.29m) |
|
Tailplane span |
11ft 0in |
(3.35m) |
|
Wheel track |
7ft
0in |
(2.13m) |
|
Wheelbase |
4ft
7in |
(1.40m) |
|
Cabin door (each) |
|
Height (mean) |
3ft
0in |
(0.91m) |
|
Width (mean) |
2ft
9in |
(0.84m) |
|
Height to sill |
3ft
6in |
(1.07m) |
|
Dimensions, Internal |
|
Cabin Length |
6ft
6in |
(1.98m) |
|
Max width |
3ft
9in |
(1.14m) |
|
Max height |
3ft
6in |
(1.07m) |
|
Floor area |
29ft² |
(2.69m²) |
|
Volume |
85ft³ |
(2.41m³) |
|
Baggage space |
15ft³ |
(0.42m³) |
|
Areas |
|
Wings, gross |
119.5ft² |
(11.10m²) |
|
Ailerons (total) |
9.2ft² |
(0.85m²) |
|
Trailing edge flaps (total) |
10.7ft² |
(0.99m²) |
|
Fin |
21.7ft² |
(2.02m²) |
|
Rudder |
6.76ft² |
(0.63m²) |
|
Tailplane |
27.5ft² |
(2.55m²) |
|
Elevators |
10.9ft² |
(1.01m²) |
|
Weights and Loadings |
|
Weight empty, equipped |
985lb |
(447kg) |
|
Max T-O weight |
1,600lb |
(725kg) |
|
Max wing loading |
13.40lb/ft² |
(65.42kg/m²) |
|
Max power loading |
16.00lb/hp |
(7.26kg/hp) |
|
Performance (at max T-O weight) |
|
Max level speed at S/L |
127
mph |
(204 km/h) |
|
Max diving speed |
195
mph |
(314 km/h) |
|
Cruising speed (75% power) at
7,000 ft |
118
mph |
(190 km/h) |
|
Econ cruising speed (60% power)
at 8,000 ft |
108
mph |
(174 km/h) |
|
Stalling speed, flaps up |
62
mph |
(100 km/h) |
|
Stalling speed, flaps down |
53
mph |
(86
km/h) |
|
|
