View attachment 484455
Spitfire I - 6.25 lb, 2600 rpm (6,050 lb)
Hurricane I - 6.25 lb, 2600 rpm (6,316 lb)
Mohawk II - 87 cm, 2550 rpm (5,962 lb)
All A&AEE tests. The Mohawk is from the Norwegian order and has an R1830-SC3G engine.
Does anyone know if there was supposed to be a difference with the R1830-SC3G engines given to France? French numbers seem to indicate critical alt was about 14,000 feet, not 10,000 feet as in the Mohawk II.
In Flying to the Limit, page 131, the British test of a Mohawk IV (H-75A-4) with 6 LMG and armor, showed best climb of 2,600 fpm at 8,000 feet. Climb rate did not fall below 1,000 fpm until 27,000 feet. 3.9 minutes to 10,000 feet. 6.2 minutes to 15,000. 8.8 minutes to 20,000. 13.3 minutes to 26,000. 18 minutes to 30,000. 23.2 minutes to 32,000. 302 mph at 14,000. Test was done in early 1941.