The British production contract stated that a maximum speed of + /-4 % was required at rated altitude.
2.
The latter system, when engaged, was capable of increasing engine output by above the rated altitude to increase high-altitude performance.
3.
The DB 605AS ( M ) improved the maximum rated altitude by using a larger supercharger taken from the DB 603 but was otherwise similar to the A ( M ).
4.
Performance of the G-1 was similar, but above rated altitude the GM-1 system it was equipped with could be used to provide an additional 350 horsepower.
5.
Maximum speed of the G-2 was 537 km / h ( 334 mph ) at sea level and 660 km / h ( 410 mph ) at 7, 000 m ( 22, 970 ft ) rated altitude with the initial reduced 1.3 atm rating.
6.
The ASM engine was built with a larger capacity supercharger, and had a higher rated altitude, and correspondingly the top speed of the G-14 / AS was 560 km / h ( 348 mph ) at sea level, and 680 km / h ( 422 mph ) at 7.5 km ( 24, 600 ft ) altitude.
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