Military Wiki
Advertisement
5-Inch Forward Firing Aircraft Rocket
5in FFAR F4U MAG-33 Okinawa Jun1945
FFARs being loaded
Type Air-to-surface rocket
Place of origin United States
Service history
Used by United States military
Production history
Produced 1943-1945
Specifications (5-inch FFAR)
Mass 80 pounds (36 kg)
Length 5 feet 5 inches (1.65 m)
Diameter Warhead: 5 inches (130 mm)
Motor: 3.5 inches (89 mm)
Warhead High explosive
Warhead weight 45 pounds (20 kg)

Engine Solid-fuel rocket
Operational
range
1 mile (1.6 km)
Maximum speed 485 miles per hour (781 km/h)
Guidance
system
None

The 5-inch Forward Firing Aircraft Rocket or FFAR was an American rocket developed during World War II for attack from airplanes against ground and ship targets.

Operational history[]

The first FFARs were developed by the U.S. Navy and introduced in June 1943. They had a 3.5-inch diameter and a non-explosive warhead, since they were used as an aircraft-launched ASW (Anti-Submarine Warfare) rocket and worked by puncturing the hull. It was accurate enough for use against surface ships and land targets, but these missions required an explosive warhead.[1] A 5-inch anti-aircraft shell was attached to the 3.5-inch rocket motor, creating the 5-Inch FFAR, which entered service in December 1943. Performance was limited because of the increased weight, limiting speed to 780 km/h (485 mph).[2] The High Velocity Aircraft Rocket, or HVAR, was developed to fix this flaw.[2]

A list of aircraft that used FFAR:

See also[]

References[]

Citations
  1. Parsch 2004
  2. 2.0 2.1 Parsch 2006
Bibliography

External links[]


All or a portion of this article consists of text from Wikipedia, and is therefore Creative Commons Licensed under GFDL.
The original article can be found at 5-Inch Forward Firing Aircraft Rocket and the edit history here.
Advertisement