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Yes. Bomber Command dispatched a Meteorological Mosquitoe to the target area in advance of the Main Force. It communicated with the Master Bomber prior to the attack. It reported cloud conditions and winds to inform changes to marking methods as well as winds for adjustments to bomb sights.Later, when they had P-51's, they would send out Weather Scouts, a flight of four Mustangs, to report on the WX in the target area and presumably unforecast winds. Of course, the WX Scouts were not adverse to bagging a few Luftwaffe aircraft that they ran across during the course of their primary mission. I think I have an article on that somewhere.
I wonder what they did for radio communications for the WX Scout missions. The SCR-522 radios the Mustangs in the ETO were equipped with normally could not reach GB from Germany, but they did stage radio relay aircraft between GB and the mainland, usually P-47's, I think.
I think the shortcoming of using a S/E fighter for WX would be that the pilot would/could not provide wind finding. The mosquito crew with a navigator could possibly have done wind finding calculations during the route to the target area. I say possibly, as I am uncertain if this was actually performed.Later, when they had P-51's, they would send out Weather Scouts, a flight of four Mustangs, to report on the WX in the target area and presumably unforecast winds. Of course, the WX Scouts were not adverse to bagging a few Luftwaffe aircraft that they ran across during the course of their primary mission. I think I have an article on that somewhere.
I wonder what they did for radio communications for the WX Scout missions. The SCR-522 radios the Mustangs in the ETO were equipped with normally could not reach GB from Germany, but they did stage radio relay aircraft between GB and the mainland, usually P-47's, I think.
The first Scout force was Scout Force (exp) based at Steeple Morden. Col Budd Peaslee brought 1st BD volunteer pilots and the 355th recruited volunteers to provide experienced fighter pilots as wingman. The ground crews and Mustangs were maintained s E Flight from each squadron. IIRC July 16 was first mission.Later, when they had P-51's, they would send out Weather Scouts, a flight of four Mustangs, to report on the WX in the target area and presumably unforecast winds. Of course, the WX Scouts were not adverse to bagging a few Luftwaffe aircraft that they ran across during the course of their primary mission. I think I have an article on that somewhere.
I wonder what they did for radio communications for the WX Scout missions. The SCR-522 radios the Mustangs in the ETO were equipped with normally could not reach GB from Germany, but they did stage radio relay aircraft between GB and the mainland, usually P-47's, I think.
The original Scout Force (Experimental) Budd Peaslee had Mosquitos as the Plan scouts when he presented to 8th AF Hq in May 1944, but they were 'unavailable' and P-51Ds were acceptable. Although the phrase 'weather scouts' was used, they were focused on two factors - 1.) weather/visibility conditons over the Primary - then Secondary targets if Primary obscured, and 2.) major weather threats such as T-Storms blocking planned route to target.This interesting. Evidently the USAAF used mosquitoes for meteorological observations.
When the US Army Air Forces flew de Havilland Mosquitos
That comment by one unit commander sums up the views of many in the US Army Air Forces on the de Havilland Mosquito, an aircraft that served the AAF in relatively small numbers, but was arguably superior to anything American makers offeredwww.key.aero
Okay so:I have written several articles on Scout Force. I think Mike Williams still carries on spitfireperformance.com
Jumping in late hereI wanted to showcase the difference between TAS (True Air Speed) compared to IAS (Indicated Air Speed)
P-51D
View attachment 591938
Stall Speed at 9611lb (4360kg) loaded weight - 110.7mph (178km/h) at Sea Level
(No flaps, level flight)
That's Wing Lift Coefficient of 1.31 CL_Max which is standard for a laminar flow wing.
With this info I can calculate the stall speed at different altitudes by changing the air density to match different altitudes.
This is the TAS it needs so it doesn't stall at altitudes with different air density.
IAS = TAS at Sea Level, however TAS has to increase to maintain same IAS stall speed due to decreasing amount of air as altitude increases.
ALTITUDE / SPEED / AIR DENSITY
Sea Level - 178km/h - 1.225kg/m3
1000m - 187km/h - 1.112kg/m3
2000m - 196km/h - 1.007kg/m3
3000m - 207km/h - 0.9093kg/m3
4000m - 218km/h - 0.8194kg/m3
5000m - 230km/h - 0.7364kg/m3
6000m - 242km/h - 0.6601kg/m3
7000m - 256km/h - 0.5900kg/m3
8000m - 272km/h - 0.5258kg/m3
9000m - 288km/h - 0.4671kg/m3
10,000m - 306km/h - 0.4135kg/m3
This is why stall speed is measured in IAS.
P-51D has 178km/h IAS stall speed but it needs to at least travel at 306km/h at 10,000m to maintain 178km/h IAS and avoid stalling. As a result of higher stall speed in TAS for all planes, as you get higher the more sluggish planes turn. Their radius of turn increases drastically and also their power output is also reduced at higher altitudes making the power to weight ratio worse and worsening the sustained turn capability.
FUN FACT:
To get into Space and leave gravitational pull of earth you need to go beyond 100,000m altitude.
If P-51D was to reach 80,000m altitude, it would have to travel at 45,800km/h TAS (Mach 37.1) to maintain 178km/h IAS in order to not stall.
This is why even jets like SR-71 Blackbird have service ceiling of 26,000m altitude.
Conclusion:
TAS = How fast you travel from point A to point B. Basically how much distance you move in set amount of time.
IAS = The airflow over your wings. You need to go faster to maintain same airflow due to decreasing amount of air as you go higher in altitude. All the TAS speeds at different altitudes = 178km/h IAS
———
Another Fact:
Every plane has a structural limit and there is a maximum limit at every altitude where the plane will fall apart at certain TAS due to the extremely high IAS.
The newer next generation jets which are suppose to reach Mach 6 will still be limited to same speed at low altitudes to earlier jets, the difference is the capability of going even higher which allows the jet to achieve greater TAS before reaching structural IAS limit of an airframe. Jet technology today is at its Apex level right now that increasing max speed is the same as saying - Increasing Service Ceiling. It's a matter of creating engines which can still operate at altitudes with ridiculously low air density which would increase service ceiling.
But only when you are in a vacuüm.Spherical cows is one of the few engineering concepts I have heard of.
C-Channel was also briefed Command Channel between Bomber Command ship (s) leading a wing and the Fighter Commander leading Groups tasked to escort.Hey MIFlyer,
re "I have read repeatedly of fighter pilots homing in on their home field beacon in GB. What were they homing in with?"
The SCR-522 had 4 channels - A,B,C,D. In the ETO channel C was generally reserved for homing on your home base.
The airbases had the multiple ground set equivalents of the SCR-522, but with higher power and mast antennae.
Channel A was normally used for air-air with local squadrons and GCI
Channel B was normally used for air-ground with local tower and other-than-local towers, and air-air with other-than-local squadrons
Channel D was generally used for air-ground with DF stations and GCI when fitted with 'pip-squeak' IFF