The First
Airborne Radar

Initial experiments, by Robert Watson-Watt and Arnold Wilkins, in 1935
demonstrated that the metal parts of an aircraft would reflect radio waves, and that these
reflections could be received and used to indicate the presence of the
aircraft by drawing a line on a CRT display. RDF (Radio Direction Finding)
was born. The UK government recognised the importance of these early
experiments and work began that culminated in the Chain Home RDF (RADAR)
defence network for the British Isles in WW2.
In early 1936 a
new line of research was commenced. This was to develop an RDF (RADAR)
system that could be fitted to an aircraft for airborne use. The Chain Home RDF initially
operated with transmitted pulses at a frequency of 6MHz and required
massive aerial towers, and equipment weighing several tons. Requirements
for an airborne system included low weight, low power consumption and
small aerials. A new approach was needed.
Such small aerials
required a high transmission frequency so that a half wave dipole would be
of the order of one or two metres maximum length. At this time a frequency
of 45MHz was at the upper limits of what was technically possible outside
the laboratory. Such high frequencies were being developed for use by a
proposed television service. Special valves such as the SP41 and EF50 were developed for high
frequency television reception.
The RDF development team
obtained a single EMI 45MHz receiver chassis for airborne development
trials. This receiver had a sensitivity greatly in excess of other
receivers at this time when operating at 45MHz. Initially a ground based
transmitter was used with an airborne receiver and ranges of up to 20km
were achieved. This was sufficiently encouraging to embark on the
production of an airborne transmitter.
A transmitter was
constructed using Western Electric 316A valves. An output power of
several hundred watts was possible in pulse operation. The pulse length
was 3 microseconds and the pulses were repeated one thousand times a
second. The period between each pulse being the time available for the
reception of any reflected signal. These trials proved encouraging and
development continued.
The frequency of operation had to
increase so that the aerial size could be reduced. A new transmitter was
constructed. This used two 316A's in push-pull. Tests at various
frequencies followed and 200MHz was chosen for the final version. To receive these Very High
Frequency (VHF) signals a converter was built for the receiver. The
original receiver on 45MHz then became the IF frequency. The front end
used acorn valves for the initial frequency conversion. This pattern of
equipment was fitted to a pair of RAF Avro Anson's and signals reflected
from ships at nearly five kilometres distance were soon
detected.
In September 1936 during a major Royal Navy
exercise the aircraft carrier Courageous was detected at a range of
approximately 10km. When the aircraft carrier launched planes to intercept
the Anson, their detection by the Anson marked the first time aircraft
reflections were seen on an airborne RADAR screen.
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