davparlr
Senior Master Sergeant
Sorry for the long intro but I thought the data would be useful
I have some questions and what-ifs about the first generation jets. Here's some data, in order of date of first flight
He-280V-1
First Flight 4/41
Empty Weight 7093
Full Weight 9415
Max Speed 510
Total Thrust 2640
Thrust to Weight .37
E.28/39
First Flight 5/41
Empty Weight 2886
Full Weight 3748
Max Speed 338
Total Thrust 860
Thrust to Weight .29
Me-262V-3
First Flight 7/42
Empty Weight 8366
Full Weight 14272
Max Speed 540 (at 3960 lb thrust so this aircraft was probably slower)
Total Thrust 3700
Thrust to Weight .44
XP-59A
First Flight 10/42
Empty Weight-lbs 7320
Full Weight-lbs 12562
Max Speed-mph 404
Total Thrust-lbs 2800
Thrust to Weight-empty .38
Meteor F.1
First Flight 3/43
Empty Weight 8140
Full Weight 13800
Max Speed 417
Total Thrust 3400
Thrust to Weight .41
Vampire DH-100
First Flight 9/43
Empty Weight 6380
Full Weight 8587
Max Speed 540 (F.1 at 3100 lb thrust)
Total Thrust 2700
Thrust to Weight .42
XP-80
First Flight 1/44
Empty Weight 6280
Full Weight 8916
Max Speed 502
Total Thrust 2460
Thrust to Weight .39
P-59A
First Flight 10/44
Empty Weight 7950
Full Weight 10822
Max Speed 413
Total Thrust 4000
Thrust to Weight .5
XFD-1
First Flight 1/45
Empty Weight 6156
Full Weight 8626
Max Speed 487
Total Thrust 3200
Thrust to Weight .5
XP-84
First Flight 2/46
Empty Weight 9080
Full Weight 13400
Max Speed 592
Total Thrust 3750
Thrust to Weight .41
The first question has to do with the P-59? If we look at the basic stats, it seems as if it should have been more successful and, a good performer. The XP-59A, with slightly more thrust than the He-280, and equivalent thrust to weight ratio, was over a 100 mph slower. Similarly, the P-59A, with the same thrust has the Me-262, was almost 130 mph slower. It appears to me that there was no good reason the P-59 was such a dog. It's got to be poor aerodynamic design. The wing root mounted engines should have been a more efficient design than the Meteor and the two German jets. I am sure that if they had been flared into the fuselage ala P-80 or FH-1, they would have improved efficiency significantly. But those wings! What were they thinking about? They are huge, larger than the P-47N, twice as large as the He-280 and 147 sqft larger than the YP-80, and most likely not a low drag airfoil. Of course I don't know what the AAF specified. I think Arnold made a mistake when he selected Bell to handle the first jet aircraft, especially since the P-39 was an underperformer. It looks like the P-59 was rushed into manufacture so fast, basic aero analysis, like inlet/engine mounting design, was not performed, and Bell seemed to have poor understanding. I think other companies would have done a better job, certainly Lockheed (who already had jet aircraft and jet engine design experience, L-133, L-1000), North American (the P-51 was already being delivered by that time), and Republic, all of which had experience in successful high performance designs, even at this early time.
What ifs.
1. What was wrong with the P-59A and, if Arnold had given the job of developing the first American jet fighter to North American, Lockheed, or Republic (which was also located near GE), could America actually have fielded a capable jet fighter in the fall of '44.
2. If Germany had the will, would/could they have had the He 280 operational in the Fall of '43, and, if so, how would the Allies reacted to its appearance on the battlefield and what would have been the impact on the war?
I have some questions and what-ifs about the first generation jets. Here's some data, in order of date of first flight
He-280V-1
First Flight 4/41
Empty Weight 7093
Full Weight 9415
Max Speed 510
Total Thrust 2640
Thrust to Weight .37
E.28/39
First Flight 5/41
Empty Weight 2886
Full Weight 3748
Max Speed 338
Total Thrust 860
Thrust to Weight .29
Me-262V-3
First Flight 7/42
Empty Weight 8366
Full Weight 14272
Max Speed 540 (at 3960 lb thrust so this aircraft was probably slower)
Total Thrust 3700
Thrust to Weight .44
XP-59A
First Flight 10/42
Empty Weight-lbs 7320
Full Weight-lbs 12562
Max Speed-mph 404
Total Thrust-lbs 2800
Thrust to Weight-empty .38
Meteor F.1
First Flight 3/43
Empty Weight 8140
Full Weight 13800
Max Speed 417
Total Thrust 3400
Thrust to Weight .41
Vampire DH-100
First Flight 9/43
Empty Weight 6380
Full Weight 8587
Max Speed 540 (F.1 at 3100 lb thrust)
Total Thrust 2700
Thrust to Weight .42
XP-80
First Flight 1/44
Empty Weight 6280
Full Weight 8916
Max Speed 502
Total Thrust 2460
Thrust to Weight .39
P-59A
First Flight 10/44
Empty Weight 7950
Full Weight 10822
Max Speed 413
Total Thrust 4000
Thrust to Weight .5
XFD-1
First Flight 1/45
Empty Weight 6156
Full Weight 8626
Max Speed 487
Total Thrust 3200
Thrust to Weight .5
XP-84
First Flight 2/46
Empty Weight 9080
Full Weight 13400
Max Speed 592
Total Thrust 3750
Thrust to Weight .41
The first question has to do with the P-59? If we look at the basic stats, it seems as if it should have been more successful and, a good performer. The XP-59A, with slightly more thrust than the He-280, and equivalent thrust to weight ratio, was over a 100 mph slower. Similarly, the P-59A, with the same thrust has the Me-262, was almost 130 mph slower. It appears to me that there was no good reason the P-59 was such a dog. It's got to be poor aerodynamic design. The wing root mounted engines should have been a more efficient design than the Meteor and the two German jets. I am sure that if they had been flared into the fuselage ala P-80 or FH-1, they would have improved efficiency significantly. But those wings! What were they thinking about? They are huge, larger than the P-47N, twice as large as the He-280 and 147 sqft larger than the YP-80, and most likely not a low drag airfoil. Of course I don't know what the AAF specified. I think Arnold made a mistake when he selected Bell to handle the first jet aircraft, especially since the P-39 was an underperformer. It looks like the P-59 was rushed into manufacture so fast, basic aero analysis, like inlet/engine mounting design, was not performed, and Bell seemed to have poor understanding. I think other companies would have done a better job, certainly Lockheed (who already had jet aircraft and jet engine design experience, L-133, L-1000), North American (the P-51 was already being delivered by that time), and Republic, all of which had experience in successful high performance designs, even at this early time.
What ifs.
1. What was wrong with the P-59A and, if Arnold had given the job of developing the first American jet fighter to North American, Lockheed, or Republic (which was also located near GE), could America actually have fielded a capable jet fighter in the fall of '44.
2. If Germany had the will, would/could they have had the He 280 operational in the Fall of '43, and, if so, how would the Allies reacted to its appearance on the battlefield and what would have been the impact on the war?