wuzak
Captain
In May 1937 George Volkert, then chief designer at Handley Page, wrote a memorandum about the design of future bomber aircraft and the influence that bombing policy would have on design.
In the introduction, he states:
He continues:
From this we can see that the high speed unarmed bomber concept pre-dated the Mosquito by several years.
In the discussion section, Volkert lays out the pros and cons of the unarmed bomber.
In the second part, Volkert puts numbers to his theories, using Specification P.13/36 as a basis.
P.13/36 had three conditions:
(a) 1,000lb bomb load with 1,000 mile range, take-off in 500 yards
(b) 2,500lb bomb load with 2,000 mile range
(c) 3,500lb bomb load, 3000 mile range and accelerated take-off (catapult)
He compared the aircraft and crew required to carry 36,000lb of bombs for loads (a) and (c).
For load case (a)
For load case (c)
Evidently he is assuming different crew requirements for the different tasks.
He concludes by saying that if the same number of bombers were used, the new bomber would carry three times the bombs and use half the crew compared to P.13/36.
He then provides a weight estimation for each type and for the loads carried.
I have only showed the main differences in the weight summary, though he also provides a calculation for tare weight.
Load Case (a)
Load Case (b)
Load Case (c)
The advantages of the "new bomber" were, according to Volkert:
In the introduction, he states:
It is the purpose of the following memorandum to show that a drastic revision of present ideas is essential if the utmost performance and destructive power is to be obtained, combined with the maximum economy in the use of highly trained personnel and highly expensive and delicate equipment.
He continues:
It has already been suggested that the future bomber will be provided with no means of self defence other than that arising out of its own very high performance.
From this we can see that the high speed unarmed bomber concept pre-dated the Mosquito by several years.
In the discussion section, Volkert lays out the pros and cons of the unarmed bomber.
- the destructive power afforded by the bomber was greater than at any time before
- that it can be deployed far more rapidly
- that bombing would most likely be against civilian targets
- precision bombing required far greater perfection of equipment and air crew skill than random bomb dropping.
- at the time of writing there was no effective counter-measure against incendiary and gas attacks. It is clear that he thought gas attacks likely.
- the training and supply of highly skilled air crew was thought to be limited. Thus the unarmed bomber with 2, or 3, crew would be more efficient in using the skill base.
- raids would use the clouds over Europe as part of their protection. It was suggested that raids would avoid concentrations of enemy fighters, and that raids would not be sent on clear days. The chance of interception of a high speed bomber operating along these lines was thought to be remote. Radar, of course, changed this.
- close formations of bombers would not be necessary, a loose formation being preferred. There would be two lead aircraft with three crew (pilot, W/T operator, navigator) while the remainder of the aircarft would have two (pilot and W/T operator/navigator). The aircraft would maintain their formation by position keeping using radio signals. Bombing would be done on a signal from one fo the leaders (as the 8th AF ended up doing)
- Vertical storage of bombs was thought better than horizontal storage, as they would remain on or near the CoG. This suggests something like the B-17's bomb bay to me.
In the second part, Volkert puts numbers to his theories, using Specification P.13/36 as a basis.
P.13/36 had three conditions:
(a) 1,000lb bomb load with 1,000 mile range, take-off in 500 yards
(b) 2,500lb bomb load with 2,000 mile range
(c) 3,500lb bomb load, 3000 mile range and accelerated take-off (catapult)
He compared the aircraft and crew required to carry 36,000lb of bombs for loads (a) and (c).
For load case (a)
P.13/36 | New Bomber | |
No. Aircraft Required | 36 | 12 |
No. Crew Required | 144 | 24 |
For load case (c)
P.13/36 | New Bomber | |
No. Aircraft Required | 10 | 5 |
No. Crew Required | 60 | 15 |
Evidently he is assuming different crew requirements for the different tasks.
He concludes by saying that if the same number of bombers were used, the new bomber would carry three times the bombs and use half the crew compared to P.13/36.
He then provides a weight estimation for each type and for the loads carried.
I have only showed the main differences in the weight summary, though he also provides a calculation for tare weight.
Load Case (a)
P.13/36 | New Bomber | |
Tare Weight (lb) | 18350 | 16447 |
Crew and Parachutes (lb) | (4) 800 | (2) 400 |
Guns (lb) | 144 | NIL |
Ammunition (lb) | 520 | NIL |
Bombs (lb) | 1000 | 3000 |
Bomb Gear (lb) | 56 | 168 |
Oxygen (lb) | 117 | 55 |
Total Military Load (lb) | 2864 | 3831 |
Petrol (UKG) | 557 | 529 |
Petrol (lb) | 4289 | 4070 |
Oil (lb) | 270 | 260 |
Total Weight (lb) | 25773 | 24608 |
Cruising Speed (mph) | 278 | 300 |
Load Case (b)
P.13/36 | New Bomber | |
Tare Weight (lb) | 18350 | 16447 |
Crew and Parachutes (lb) | (6) 1200 | (3) 600 |
Guns (lb) | 144 | NIL |
Ammunition (lb) | 520 | NIL |
Bombs (lb) | 2500 | 5000 |
Bomb Gear (lb) | 140 | 250 |
Oxygen (lb) | 262 | 120 |
Total Military Load (lb) | 5069 | 6254 |
Petrol (UKG) | 1075 | 1018 |
Petrol (lb) | 8280 | 7850 |
Oil (lb) | 432 | 4151 |
Total Weight (lb) | 32131 | 30966 |
Cruising Speed (mph) | 275 | 297 |
Load Case (c)
P.13/36 | New Bomber | |
Tare Weight (lb) | 18350 | 16447 |
Crew and Parachutes (lb) | (6) 1200 | (3) 600 |
Guns (lb) | 144 | NIL |
Ammunition (lb) | 520 | NIL |
Bombs (lb) | 3500 | 7000 |
Bomb Gear (lb) | 196 | 350 |
Oxygen (lb) | 262 | 120 |
Total Military Load (lb) | 6125 | 8354 |
Petrol (UKG) | 1605 | 1515 |
Petrol (lb) | 123660 | 11670 |
Oil (lb) | 630 | 595 |
Total Weight (lb) | 37465 | 37066 |
Cruising Speed (mph) | 273 | 295 |
The advantages of the "new bomber" were, according to Volkert:
- A more aeroduynamically refined fuselage
- Minimmal protrusions on outer surface
- The wing can be mounted to the fuselage at the optimum point for reduced drag
- Thinner wing (18% vs 21% for P.13/36)
- Lighter weight due to no turrets, simplified structure, no crew access required in the fuselage, etc, allowing for an increased bomb load
- Lighter weight improves manoeuvrability
- Better crew accomodation and comfort helps the crew become more efficient
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