Hockaday CF-130 Comet

Hockaday Aircraft Corp. was established by Noel R. Hockaday in 1937 in Burbank, California. In 1939, the company tested the experimental high-wing monoplane Noelcraft (NX18933) with a 100-hp Allied Monsoon engine.

However, further development was halted due to the outbreak of World War II.

Origins and Initial Development

Work on the aircraft resumed in 1944. The refined aircraft, redesignated as the Hockaday CF-130 Comet, first flew in June 1944.

Technical Specifications of the Comet

It was a two-seat, strut-braced high-wing monoplane. It was equipped with a 130 hp Franklin 6AC engine. A 125 hp six-cylinder Continental C-125 could be used as an alternative powerplant.

The Hockaday Comet successfully passed its tests but did not enter series production.

Technical Specifications

Modification	Comet
Wingspan, m	10.06
Aircraft length, m	6.76
Aircraft height, m	3. 50
Wing area, m2	14.50
Empty weight	432
Maximum takeoff weight	726
Engine type	1 Piston engine Continental C-125
Power, kW	1 x 125
Maximum speed, km/h	230
Cruising speed, km/h	210
Practical range, km	800
Max. rate of climb, m/min	348
Practical ceiling, m	5800
Crew, crew	2

Image and diagram gallery of the Hockaday CF-130 Comet

Hockaday CF-130 Comet	Hockaday CF-130 Comet
Hockaday CF-130 Comet	Hockaday CF-130 Comet
Hockaday CF-130 Comet	Hockaday CF-130 Comet