Copyright 2007 by Brandon Cope
 
 

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General Aircraft ST-25 Jubilee

The ST-25 was part of a progressive development of twin-engine monoplanes by General Aircraft in Britain in the 1920’s and 30’s. The ST-25 was a twin-engined monoplane with fixed landing gear and first flew in 1935. It was named “Jubilee” in honor of King George V’s Silver Jubilee in 1935. Thirty were built. The fourth passenger seat at the rear of the cabin could be folded and used for additional cargo space instead.

The ST-25 burns 6.4 gallons of fuel per hour at routine usage.

Subassemblies: Heavy Fighter chassis +3, Heavy Fighter Wings +2, 2¥Small Weapon engine pods 1-2 +1, three fixed wheels +0
P&P: 2¥71-kW aerial HP gas engines with 2¥71-kW old prop [Pods 1–2] and 63-gallon tanks [Wings]
Occ: 1 CS, 4 PS     Cargo: 2.9 Body
 
Armor F R/L B T U
All 2/2C 2/2C 2/2 2/2C 2/2C

Equipment
Body: Medium radio receiver and transmitter, navigation instruments, autopilot.

Statistics
Size: 25'x40'x8' Payload: 0.49 tons Lwt: 1.43 tons
Volume:  224 Maint.: 72 hours Price: $7,600

HT: 12
HP: 130 [body], 40 [each wing], 13 [each wheel], 23 [each Pod]
 
aSpeed: 131 aAccel: 2 aDecel: 29 aMR: 5 aSR: 2
Stall: 53 mph

Design Notes
Design aSpeed is 133 mph; the historical speed, as well as actual wing area (217 sf), has been used. The cost, weight and HPs of the chassis, wings, and pods were divided by two to lower overall weight. Even so, loaded weight was reduced by a further 12% to match historical weight.

Variants
The Universal (1936) was identical in game terms, but replaced the single tailfin with twin rudders to improve instability in case of the loss of an engine. Twenty-nine were built.