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Four versions of the Pup were produced by Beagle: the Pup-100 fully aerobatic light aircraft with accommodation for two adults and powered by a 74.5kW Rolls-Royce/Continental O-200-A flat-four engine, deliveries beginning in April 1968; the Pup-150 with seating for two adults but with an optional seat for a third adult or two children and powered by a 112kW Lycoming O-320-A2B engine; the Pup-160 with a 119kW Lycoming O-320-D2C engine; and the Pup-200 with a 149kW Continental engine. A total of 128 Pups had been delivered by the close of 1969, when a further 267 aircraft were on order. However the company went into liquidation and the Pup was developed into the Bulldog by Scottish Aviation.
| CREW | 2 |
| PASSENGERS | 1 |
| ENGINE | 1 x RR/Cont. O-2001, 74kW |
| WEIGHTS |
| Take-off weight | 680 kg | 1499 lb |
| Empty weight | 418 kg | 922 lb |
| DIMENSIONS |
| Wingspan | 10.1 m | 33 ft 2 in |
| Length | 7.1 m | 23 ft 4 in |
| Height | 2.3 m | 7 ft 7 in |
| Wing area | 12.0 m2 | 129.17 sq ft |
| PERFORMANCE |
| Max. speed | 225 km/h | 140 mph |
| Cruise speed | 222 km/h | 138 mph |
| Ceiling | 2000 m | 6550 ft |
| Range | 800 km | 497 miles |
| ARMAMENT | 260kg of bombs |
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