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That is why it was used for a couple of missions by 4 aircraft across the channel.I felt like doing some math...
So this is what I come up with, using those 2 charts posted and I used very conservative numbers except for take off weight, I used the fully loaded 8000 pounds, no wind condition to assume IAS will equal ground speed (for simplicity).
Start with 120 gallons (per the expert). Take away 20 gallons for warm up per the chart and you start with 100 gallons.
Take off at S/L, climb to 25,000 feet - 140 mph indicated, 31.2 gallons used, 29.9 minutes in the air at 140 mph so we traveled 70 miles.
68.8 gallons left.
In the cruise chart there is no data for 25,000' so we'll use 20,000'
Cruise 15 minutes, 160 MPH, 8.75 gallons used - 39 miles
60.1 gallons left.
Combat! 15 minutes. 10 minutes full power, 5 minutes WEP
34.75 gallons used. We'll also assume this was a traveling fight at 300mph - 75 miles
25.35 gallons left
Fight is over, descend down to 3000' (good cruising altitude) descend 1000' per minute at 160 mph 22 minutes, 12. 8 gallons used, 58 miles
12.6 gallons left.
10 gallons reserve, 2.55 gallons left. At 160 mph you'll burn that up in about 5 minutes, 40 miles
Total mission miles with 10 gallons reserve - 282 miles
I didn't account for blower setting, auto rich or lean or density altitude, just read the data straight off the charts. OK folks, check my math!
I'm assuming that if there is no figure for a certain altitude for a certain cruise condition, it's because that throttle setting would not permit sustained operation there?
Because you can operate at that altitude at max continuous.
OK folks, check my math!
LET'S DO THE CORSAIR!!!
237 Gallons
Using max weight per the flight manual 14,200 pounds
Warm up and take off fuel consumption included per the flight manual chart.
Take off at S/L, climb to 25,000 feet - *125 knots indicated, 83 gallons used, 19 minutes in the air at *143.8 mph = 45 miles
159 Gallons left
Cruise 15 minutes, 14.5 gallons at *191mph ( *based on Report No. 6195 April 1, 1943 from Chance Vought. NAVAIR bases charts on endurance) = 47.7 miles
144.5 Gallons left
Combat! 15 minutes. 10 minutes full power, 5 minutes WEP 88 gallons at 380 mph = 94 miles NOTE: Military power used 275 GPH low blower per my manual (numbers were shown)
56.5 Gallons left
Fight is over, descend down to 3000' (good cruising altitude) descend 1000' per minute at 191 mph 22 minutes, 15.9 gallons used, 70 miles
40.6 Gallons left
Minus 10 gallons reserve -
30.6 Gallons left
40 minutes left in the air at 191 mph = 127 miles
384 miles
View attachment 624443
View attachment 624444
Methinks I'm gusting perilously close to the definition of insanity.
That's all well and good, Joe....but we all know that, in a couple more pages of this thread, the P-39 will magically be comparable to the F4U Corsair again thanks to P-39Expert's calculations and/or considered opinion.
It's kinda sad that some of us, self included, hope for a different result. Methinks I'm gusting perilously close to the definition of insanity.
Those charts are full of data. How is a layman supposed to interpret them? Be nice if someone could start a new thread with a tutorial.
Otherwise a layman may just take the most impressive number from whatever convenient column to prop up his argument.
For example, what is the difference between a combat climb and a ferry climb?
And there would have been a reason for reducing it in the rest. Then P39 needs to be clear if the performance figures are with the 120 or 90 US Gal, and prove it of courseTo be fair, the first ~160 production P-39N-1 were still fitted with the normal P-39 fuel tankage for 120 USgal.
When I did those calculations I tried to be as conservative as possible to show minimal fuel consumption so we can determine range, especially for the P-39 but the charts from the flight manual speak for themselves. I wanted to show the source instead of flapping numbers without a mention of fuel consumption. As I was doing the calculations it became apparent that a mission to 25,000' was not the best profile for the P-39And there would have been a reason for reducing it in the rest. Then P39 needs to be clear if the performance figures are with the 120 or 90 US Gal, and prove it of course