I wish that posters who insert articles would actually read them themselves
My point exactly.
The citations used for the OP:
(webmasters note: It is generally believed that the A4/V2 was not an
effective weapon because it was not accurate enough to hit an exact
target. While pinpoint accuracy was not associated with the V2, it was
much more accurate than generally reported. Not every batterie received
or installed the Leitstrahl-Guide Beam apparatus, which, was crucial to
the greater accuracy of the weapon. In the later stages of the war the
accuracy improved greatly, sometimes to within meters of the target.)
In WWII, a B-17 with the Norden Bomb Site had a 3,300' circular error
of probability (CEP), which means to absolutely guarantee a target kill
you had to drop 9,000 bombs from 1,000 bombers...which put more than
10,000 airmen at risk. In Korea, an F-84F had a 1,000' CEP, which means
to absolutely guarantee a target kill you had to drop 1,100 bombs from
550 fighters...which put 550 airmen at risk. In SEA, an F-4 had a 400'
CEP, which means to absolutely guarantee a target kill you had to drop
176 bombs from 30 fighters...which put 60 airmen at risk.
In the fall of 1944, only seven per cent of all bombs dropped by the
Eighth Air Force hit within 1,000ft of their aim point; even a
fighter-bomber in a 40 degree dive releasing a bomb at 7,000 ft could
have a circular error (CEP) of as much as 1,000 ft. It took 108 B-17
bombers, crewed by 1,080 airmen, dropping 648 bombs to guarantee a 96
per cent chance of getting just two hits inside a 400 by 500 ft area (a
German power-generation plant.)
VOL. 4, NO. 3 J. GUIDANCE AND CONTROL MAY-JUNE 1981
History of Key Technologies AIAA 81-4120
1981 Developments in the Field of Automatic
Guidance and Control of Rockets
Walter Haeussermann
The Bendix Corporation, Huntsville, Ala.
AIAA 2001-4288
The Pendulous Integrating Gyroscope
Accelerometer (RIGA) from the V-2 to
Trident D5, the Strategic Instrument of Choice
R.E. Hopkins
The Charles Stark Draper Laboratory, Inc.
Cambridge, MA
Dr. Fritz K. Mueller, Dr. Walter Haeussermann
Huntsville, AL
Also, the OP stated that the original guidance system did not allow for a tight CEP radius whereas later systems were improved considerably.
But we better not discuss the V-2 anymore, because aparently this thread is only for piloted aircraft (so no V-2, V-1 or TDR-1 talk...)