I did a quick work up on the 801D using the USN/USAAF test data as the starting point.
The data I have gives 1755 hp @ 3250 ft (I'm calling it 3280 ft, or 1 km) & 1.42 ata.
That works out to a blower pressure ratio of 1.60:1, naturally giving 1.60 ata @ SL. So that gives a SL static max of 1.60 ata, 1955 hp +- 1%. Call it about 1980 hp, about 2010 ps (1980 * 1.014).
With ram 1.65 ata should be easily attainable at SL, giving about 2070 ps (1.65/1.60 * 2010), but that is before taking ram heating into account.
We will make this easy and do it at 200 mph TAS:
200/100 ^ 2 = 4 C temp increase
SL temp is 288.36 C, rammed temp is 292.36
sqrt (288.36 / 292.36) * 2070 = 2055 ps
But, another but

, C3 injection should lower charge temp anywhere from 10 to 25 C.
At 10 C decrease:
sqrt (302.36 / 292.36) * 2055 = 2090 ps
At 25 C decrease:
sqrt (317.36 / 292.36) * 2055 = 2140 ps
So, rammed performance of 1.65 ata, 2100 ps with C3 injection is just doable at SL, when rammed. Unrammed should be about 2010 ps 1.60 ata, or about 1985 ps at the 1.58 ata given in other figures.
Greg Shaw