3.5-Inch Forward Firing Aircraft Rocket

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For other rockets with the same acronym, see 5-Inch Forward Firing Aircraft Rocket and Mk 4/Mk 40 Folding-Fin Aerial Rocket.
3.5-Inch Forward Firing Aircraft Rocket, 3.5" FFAR
FFAR being loaded on TBF.png
3.5-inch FFARs being mounted underwing on a TBF Avenger
Type Anti-submarine rocket
Place of origin USA
Service history
Used by United States Navy
Production history
Produced 1943–1944
Specifications (3.5-inch FFAR)
Weight 54 pounds (24 kg)
Length 4 feet 7 inches (1.40 m) total = 45 inches (1,100 mm) motor length + 10 inches (250 mm) steel warhead length
Diameter motor 3.25 inches (83 mm), solid steel warhead 3.5 inches (89 mm)
Warhead None

Engine Caltech solid-fuel rocket
2,300 lbf (10.4 kN)
Operational
range
1,500 yards (1,400 m) nominal firing range
Speed 1,045 miles per hour (1,682 km/h) = 1,180 feet per second (360 m/s) rocket delta V plus + 240 miles per hour (390 km/h) approx. aircraft speed
Guidance
system
None

The 3.5-Inch Forward Firing Aircraft Rocket, or 3.5-Inch FFAR, was an American rocket developed during World War II to allow aircraft to attack enemy submarines at range. The rocket proved an operational success, and spawned several improved versions for use against surface and land targets.

Design and development[edit]

Following trials by the Royal Air Force of rocket-propelled, air-launched weapons for anti-submarine warfare during 1942, the United States Navy launched a high-priority project during the summer of 1943 for the development of an anti-submarine rocket of its own.[1]

The resulting rocket was a simple design with four tail fins for stabilization at the rear,[1] powered by a rocket motor that had been under development by Caltech since 1943.[2] The warhead contained no explosive. The rocket's nose was a solid steel mass, weighing 20 pounds (9.1 kg), that punctured the pressure hull of a target submarine through the kinetic energy and momentum from its high velocity and mass.[3] The nose of the 3.5" FFAR was given a relatively blunt conical shape that had been shown experimentally to give a maximum pitch-up of the nose as the rocket entered the water. This caused the rocket to shoot forward at a shallow depth deadly to submarines that were surfaced or traveling at snorkel or periscope depth.[4] The rockets were launched in a shallow dive, since entry into the water at too steep an angle would defeat their ability to shoot forward at the required shallow depth. The rocket remained lethal even after passing through up to 130 feet of water, giving the pilot a target several times the actual size of the submarine. The sweet spot for targeting was considered to be 60 feet in front of the near side of the submarine. Typical firing range was about 1500 yards.[5]

Operational history[edit]

Following expedited development, the weapon, officially designated the 3.5-Inch Forward Firing Aircraft Rocket, entered operational service with the U.S. Navy late in 1943;[1] production of 10,000 rockets per month had been ordered that August.[6] The FFAR's first "kill" of an enemy submarine took place 11 January 1944. The rocket was originally carried by the TBF Avenger torpedo bomber. Excessive drag caused by the original 92" long channel-slide launchers was largely eliminated with the introduction of zero length launchers in May 1945.[3] Zero length launchers quickly became standard on most fighters and many light bombers for firing a variety of rockets with 3.25" or 5" diameter rocket motors.

Although the rocket's accuracy was more than sufficient to allow usage against surface targets, the narrow body diameter restricted the size of any explosive warhead that could be fitted.[1] Therefore, for use against ships and land targets, the rocket was given a warhead consisting of a 45 lb re-fused 5" Mark 35 artillery shell, producing the 5-Inch Forward Firing Aircraft Rocket, usually shortened to 5" AR.[3][7]

See also[edit]

References[edit]

Citations
  1. ^ a b c d Parsch 2004
  2. ^ von Braun and Ordway 1975, p.98.
  3. ^ a b c Campbell 1985, p.170.
  4. ^ C. W. Snyder, Caltech's Other Rocket Project: Personal Recollections, pp. 7-10, Engineering & Science, Spring 1991
  5. ^ E.W. Price, C.L. Horine, and C.W. Snyder (July 1998). "EATON CANYON, A History of Rocket Motor Research and Development in the Caltech-NDRC-Navy Rocket Program, 1941-1946,". 34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Cleveland, Ohio. AIAA.
  6. ^ Friedman 1982, p.198.
  7. ^ Parsch 2006
Bibliography

External links[edit]

Media related to FFAR rockets at Wikimedia Commons