davparlr
Senior Master Sergeant
I have always wondered about the large gap in performance of US heavy bombers in WW2. There seems to be a generation missing.
1st generation
B-17G
Gross weight 55,000 lbs
Range 2000m w/6k bombs
Max speed 287mph at 25k ft
Cruise speed 182 mph
Ceiling 35,600 ft
Operational altitude 20-25k
Engines turbocharged R-1820 1200 hp at 25k
Original operations Apr 38
B-24H
GW 56,000 lbs
Range 2100m w/5k bombs
Max Speed 290 mph at 25k ft.
Cruise speed 215 mph
Ceiling 28,000 ft.
Operational altitude 20-25k
Engines turbocharged R-1830 1200 hp at 25k
Original operations 1941
3rd Generation
B-29A
GW 140,000 lbs
Range 4100 mi w/16k bombs
Max Speed 357 mph
Cruise speed 220 mph
Ceiling 33,600
Operation altitude 30k
Engines turbocharged R-3350 2200 hp at takeoff
Original operations May 44
It seems to me the AAF jumped a capability level when they went directly to the B-29. The AAF did plan on developing a generation two, the XB-33A, but cancelled it to concentrate on the B-29. Risk could have been low in that it used the proven R-2600 and could have been designed without pressurization. The plane could ingress and egress at 242 mph and 25-30k (using pressure breathing?) and have a dash speed of 250-300 mph over the target area. Bombing error would have increased but this would be alleviated by a 10,000 lb bomb load. High altitude would reduce Flak coverage and speed would reduce exposure. For an eight hundred mile ingress-egress, exposure would have been reduced about 36 minutes. At the higher altitude and faster speeds, interceptors would have less closure speed and poorer maneuverability than when opposing B-17/24s. Technical difficulties hampered the B-29 continuously such that the obsolete B-17 and B-24 labored on until the end of the war.
Proposed 2nd Generation
B-33A
GW 95,000 lbs
Range 2,000 mi w/10k bombs
Max speed 345 mph
Cruise speed 242 mph
Operational altitude 25-30k non-pressurized, 30+ pressurized
Engines four Wright R-2600-15, 1800 hp each
Proposed Operational early Summer, '44
In 1944, the bomber could be updated with turbocharged R2800-21(water injection), flat rated 2300 hp (combat) to 27,000 ft, 2000 hp (Mil) and 1625 hp (normal) to 25,000 ft., and pressurized with a top speed of 370+ mph and a cruise speed of 255 mph cruise, and operational altitude 30-35k.
I guess my question is how many lives could have been saved had something like the B-33A been fielded in mid-43. Another question would be was the B-33A a possible threat to the B-29 such that it was terminated for political purposes?
1st generation
B-17G
Gross weight 55,000 lbs
Range 2000m w/6k bombs
Max speed 287mph at 25k ft
Cruise speed 182 mph
Ceiling 35,600 ft
Operational altitude 20-25k
Engines turbocharged R-1820 1200 hp at 25k
Original operations Apr 38
B-24H
GW 56,000 lbs
Range 2100m w/5k bombs
Max Speed 290 mph at 25k ft.
Cruise speed 215 mph
Ceiling 28,000 ft.
Operational altitude 20-25k
Engines turbocharged R-1830 1200 hp at 25k
Original operations 1941
3rd Generation
B-29A
GW 140,000 lbs
Range 4100 mi w/16k bombs
Max Speed 357 mph
Cruise speed 220 mph
Ceiling 33,600
Operation altitude 30k
Engines turbocharged R-3350 2200 hp at takeoff
Original operations May 44
It seems to me the AAF jumped a capability level when they went directly to the B-29. The AAF did plan on developing a generation two, the XB-33A, but cancelled it to concentrate on the B-29. Risk could have been low in that it used the proven R-2600 and could have been designed without pressurization. The plane could ingress and egress at 242 mph and 25-30k (using pressure breathing?) and have a dash speed of 250-300 mph over the target area. Bombing error would have increased but this would be alleviated by a 10,000 lb bomb load. High altitude would reduce Flak coverage and speed would reduce exposure. For an eight hundred mile ingress-egress, exposure would have been reduced about 36 minutes. At the higher altitude and faster speeds, interceptors would have less closure speed and poorer maneuverability than when opposing B-17/24s. Technical difficulties hampered the B-29 continuously such that the obsolete B-17 and B-24 labored on until the end of the war.
Proposed 2nd Generation
B-33A
GW 95,000 lbs
Range 2,000 mi w/10k bombs
Max speed 345 mph
Cruise speed 242 mph
Operational altitude 25-30k non-pressurized, 30+ pressurized
Engines four Wright R-2600-15, 1800 hp each
Proposed Operational early Summer, '44
In 1944, the bomber could be updated with turbocharged R2800-21(water injection), flat rated 2300 hp (combat) to 27,000 ft, 2000 hp (Mil) and 1625 hp (normal) to 25,000 ft., and pressurized with a top speed of 370+ mph and a cruise speed of 255 mph cruise, and operational altitude 30-35k.
I guess my question is how many lives could have been saved had something like the B-33A been fielded in mid-43. Another question would be was the B-33A a possible threat to the B-29 such that it was terminated for political purposes?