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The problem is that even knowing that the ports of the South Coast were full of vessels and knowing that an invasion was imminent doesn't tell you where the landings will be made.
Yeah, a biplane during WWICoventry Ordnance Works made an Airplane?
Yes, which is why checking recon results with the transponders against the reports from intelligence agents would potentially expose the nature of the double agents in play. (in spite of the firm insistence that such was impossible)From what I read when the (accurate) results from the transponders disagreed with the (inaccurate) on the ground reports they believed the false reports, presumed the transponders were not working and stopped using them.
Typo there with the V2, but otherwise very neat. I'd missed wiki's small article on the 005 until now: Porsche 109-005 - Wikipedia, the free encyclopediaA Porche design, the 109-005 and a BMW design, the P3006. Both 2 hour life disposable. The 109-005 designer was Max Mueller, who had joined from Heinkel Hirth.
The V2 required 280 man-hours to build, maybe 400 with autopilot. A BMW 003 required 700 hours, less than a piston engine, a disposable engine less again. A turbojet powered V1 would not cost much more than a pulse jet V1. German manned jet engine designs were preparing 2 hour life disposal steel turbine blades if they ran out of refractory alloys.
I'd not heard that at all before, either the higher thrust or higher test speed. Do you have any more specifics? That's the sort of performance gain I'd expect to see with a decent thrust augmentor (or cowling to similar effect -using ram air ducted around the hot section of the engine, deriving energy from the waste heat before being exhausted along with the combustion jet -in practice, a simpler, lighter thrust augmentor attached just aft of the exhaust nozzle is more effective at low speeds, simpler and lighter -the ram effect of a longer sleeve type duct/cowl may be more significant at higher speeds). Sleeve type ducts have the added advantage of working as heat shields around the very hot body/exhaust pipe of pulse jets. (significant for say, underwing mountings)The V1 also known as the Fiesler Fi 103, Kirschkern (Cherrystone, its code name) was to be guided.
Standard propulsion was the Argus Reed Valve Pulse Jet. Speed was 390mph at low altitude. Improvements in the engine let experimental V1 achieve 515mph at low altitude in Feb 1945
All very interesting, though I still wonder if improved guidance systems could have been developed earlier if the vibration/thrust/fuel consumption limitations of the pulse jet engine hadn't been a constraining factor. (plus development of a reliable, reasonably well performing pulse jet -in practice it's more an art than engineering and involves to this day a lot of trial and error rather than calculated engineering -best option with starting from scratch is to make dozens of prototypes all at once with minor to major differences across the board, some variables even chosen at random to study the behavior ... and then hope the results scale up well) Valve design was probably the most consistent, conventional mechanically engineerable component of the As 014.The disposable turbojet allowed a longer range; increased speed and its lack of vibration did not disturb the guidance system.
Ewald I guidance couldn't alter the path of the V1 once launched. However a second generation system called Ewald 2 could.
There were two terminal homing warheads "Raddischien" or Radish for homing on the allied radar and guidance beacons (tested on a BV246 glide bomb) and MAX-P for homing on to allied microwave systems that might be used in the V1.
A V1 with turbojet, extra fuel and Ewald II guidance might have been launched against Britain from bases in Germany. The range of a radio guidance system is determined by the radar horizon: the higher one goes the further the horizon.
Indeed, similar strategies to what RAF Bomber Command had formally adopted under Harris. (targeting material -civil and military, intellectual, and physical/bodily labor forces and infrastructure)Area Bombardment, as Arthur Harris plainly explained in his memoir about the targeting bombing of Lubeck, meant that no specific target was chosen, the geometric centre of the city was chosen and destroyed by concentrating in enough bombs, incendiaries in a short enough time to create a fire storm. The true meaning of the terms 'dehousing' and 'demoralisation' should be clear.
Koopernic
where you got your quote? The first use of H2S was about one year (Jan 43) after area bombing decision. "Coventry Ordnance Works produced 25% of Britain's aircraft" Really? Lübeck had a port and production connected to U-boats, Rostock had a port and two aircraft factories, Arado's and Heinkel's. Was that so different from e.g. Bristol, which had a port and an a/c factory (Bristol) and was heavily bombed during 40-41 Blitz? Or didn't British have "cultural areas", only Germans? To what are you aiming at?
I was on a team that restored a pulsejet for the Planes of Fame. We had 10 people researching the V-1 not including the 3 team members and we never uncovered a 515 mph V-1 of any sort.
So, I'd be interested in that if you could point me to a source that I can obtain and study. I see the 390 mph above but wartime production V-1s usually cruised more around 360 - 375 mph as far as we could uncover from German documents.
If you want to see our results, search Goolge Video for Chino Pulsejet. We also filmed one night run and it is interesting. There was no manual and it took us about a year to figure out how to start it and then another month and a half before we figured out how to get it from idle to full power. We ran it on both 87 Octane unleaded and 100 Octane unleaded. It preferred 87 Octane fuel and ran just fine. 2.2 gallons per minute at idle and 3.3 gallons per minute at full power. We only ran ours untl the internal temperature got to 1,100°F and then shut it off to save the reed pedals. That gave us about a 1.5 minute run while standing still and the temp was down by some 300°F when we ran down the runway at maybe 25 mph. Interestingly enough, the small forward speed combined with the new cowling we made increased thrust by about 25%. We had a thrust measuring setup on the test stand using a spring with a know spring constant and a linear hydraulic cylinder to get the spring compression. We calibrated it to about ±1%. The principle in that restoration was Robin Scott. Bob Velker and I helped Robin for about the last 6 months and all the duration of the time we discovered how to start and operate it.
Neat! I'd seen the Chino pulse jet demonstrations before, but hadn't realized the nature of the cowling.If you want to see our results, search Goolge Video for Chino Pulsejet. We also filmed one night run and it is interesting. There was no manual and it took us about a year to figure out how to start it and then another month and a half before we figured out how to get it from idle to full power. We ran it on both 87 Octane unleaded and 100 Octane unleaded. It preferred 87 Octane fuel and ran just fine. 2.2 gallons per minute at idle and 3.3 gallons per minute at full power. We only ran ours untl the internal temperature got to 1,100°F and then shut it off to save the reed pedals. That gave us about a 1.5 minute run while standing still and the temp was down by some 300°F when we ran down the runway at maybe 25 mph. Interestingly enough, the small forward speed combined with the new cowling we made increased thrust by about 25%. We had a thrust measuring setup on the test stand using a spring with a know spring constant and a linear hydraulic cylinder to get the spring compression. We calibrated it to about ±1%. The principle in that restoration was Robin Scott. Bob Velker and I helped Robin for about the last 6 months and all the duration of the time we discovered how to start and operate it.
See my reply here: http://www.ww2aircraft.net/forum/av...s-ww2-jets-39511-post1200914.html#post1200914The He280 was intended to have the HeS8 as it's powerplants...and the ones tested and demonstrated with the HeS8 performed to all expectations. It was the HeS30 that was supposed to replace the HeS8
Lubeck was a coastal city, so of course it had a port. There was a medium size slipway that repaired Baltic Sea fishing vessels. It sometimes handled repairs to smaller mine sweepers. No U-boats that I know of.
Coventry Ordinance works, I believe the correct statement should be produced parts for 25% of Britain's aircraft.
The first multicavity magnetron that the Germans got their hands on was from a December 1942 crashed Stirling near Rotterdam. The magnetron was analysed but subsequently bombed and destroyed but by then another had been captured in January 1943. Gee and Oboe (accurate to the radar horizon) were available well before this time.
The point is Lubeck's population was targeted and bombed not the slipway or the Draeger works for medical gases which also did rebreather cartridges for frogmen. the slipway wasn't specifically targeted with the nearby civilians killed as a result of collateral damage due to aiming limitations or a desire to destroy nearby transportation. The civilians themselves were as much if not more the target.
Bomber command maintained a list of legitimate targets in cities that were subjected to Area Bombardment as defence against possible war crime charges by its aviators.
Below a "AWACS" Vickers Wellington which might have been used to use a compass pointed aerial to provide oboe pulse signals transmissions and reception to targets area far greater than the normal radar horizon. The timing pulses would need to be corrected to allow for the movement of the aircraft around a base station but the British electronics engineers were rather good at timing circuits.
Yes, which is why checking recon results with the transponders against the reports from intelligence agents would potentially expose the nature of the double agents in play. (in spite of the firm insistence that such was impossible)
That would be a far bigger and more valuable revelation than anything regarding accurate reports on V1 bombing impacts.