... which crashed in 1948.

A bit of the accident report below.
Link here:
http://www.fightercontrol.co.uk/forum/v ... 94&t=78756Place of Accident - Ohio, Montgomery, Dayton 8 miles North
Nearest Airfield - Wright Field
Date - 19th August 1948
Plane Serial - 44-63528
Plane Type - F-51D
Date of Manufacture - 20th November 1944
Total flying Hours - 341.15
Last Overhaul - New
Operator - 1st Lieutenant Paul L. Chell of the USAF
Unit - Flight Test - Fighter Operations Section
Flying Experience of Operator 1641.4 hours total, 286.4 hours on this type, 61.05 hours on this plane, with 125.4 hours in the last 90 days
Special equipment carried on plane:
'This particular F-51D was equipped with one ramjet engine on each wing tip. Each jet used fuel only from left and right wing tanks respectively. The electrical equipment for each engine (Boost pump, solenoid shut off etc) was located immediatety outboard of the wing tanks, behind the gun ports. Since the fire started in this section it is believed that a combination of an electrical spark and leaking fuel was the exact cause of the accident'
Ramjet Performance:
The ramjet was build by a company called Marquardts and was a subsonic design of 20 inch diameter.
The F-51D obtained a speed increase of 40 mph (approx 9%) when in use, increasing top speed from 437 to 480 mph. Whilst not much, it must be remembered that the ramjet weighed only 100 lbs and produced 10 times its own thrust, i.e. 1,000 lbs of thrust
Pilots statement:
'Takeoff was approximately 1430 on the 19th August 1948. Takeoff was normal. Tests were being run as prescribed by the project engineer. After approx 15 minutes of normal Jet operation, the right jet flamed out. A normal restart was made. After one of two minutes of operation, the right jet flamed out again. Just as another restart was being made, a severe explosion was heard. The explosion occured inboard of the ramjet and either on the bottom or inside the wing. Lateral control was nearly impossible and almost immediately flames were observed inside the wing about a foot or two from the wing root. Fuel was turned off, power reduced, and the airplane was brought to a stall attitude. The canopy was then released and egress made from an inverted position.
Paul L. Chell, 1st Lt, USAF'
The plane crashed into a wooded area burning brush for about 100 foot radius, and here are the photos from the crash report.

