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CRV7
The CRV7, short for "Canadian Rocket Vehicle 7", is a 2.75-inch (70 mm) folding-fin ground attack rocket produced by Bristol Aerospace in Winnipeg, Manitoba. It was introduced in the early 1970s as an upgraded version of the standard U.S. 2.75-inch air-to-ground rocket. It was the most powerful weapon of its class, the first with enough energy to penetrate standard Warsaw Pact aircraft hangars. The CRV7 remains one of the most powerful air-to-ground attack rockets to this day, and has slowly become the de facto standard for Western-aligned forces outside the United States. Beginning in 2021, 83,303 stored Canadian CRV7s are slated for disposal, having been removed from service from 2005 to 2007. In 2024 the Department of National Defence was considering donating the rockets to Ukraine as military aid to defend against the Russian invasion of Ukraine. An estimated 8,000 rockets have functioning warheads, while the remainder could be used for parts or modification. In September 2024 Canadian defence minister Bill Blair announced Canada would be sending 80,840 rocket motors to Ukraine over the next months, in addition to the 2,100 already shipped, along with 1,300 warheads.
The CRV7 was an offshoot of late 1950s research at CARDE (now DRDC Valcartier) into high-performance solid fuel rockets, research performed as a part of a general program studying anti-ballistic missiles. With Aerojet's assistance, CARDE and Bristol developed the "Propulsion Test Vehicle" to test new fuel and engine designs. This program led to the development of the Black Brant sounding rocket, which first flew in 1960 and has had a long and successful career since then. Engineer Jose Tharayil from Bristol Aerospace is considered the driving force behind the CRV7's development and production.
In the early 1970s, CARDE and Bristol decided to use the same propellant and engine design for a new 2.75-inch rocket to equip the Canadair CF-104 Starfighter. The resulting RLU-5001/B (C-14) engine was first delivered by Bristol in production form in 1973. It had a total impulse of 2,320 lbf·s (10.3 kN·s) and a burn time of 2.2 seconds. The empty weight of the rocket is 6.6 kg, and it is normally equipped with a 10 lb (4.5 kg) high-explosive warhead taken from U.S. rockets.
Compared to the U.S. Mk 40 FFAR Mighty Mouse rockets the CRV7 replaced, the higher energy fuel and newer fuselage design led to a longer and much flatter trajectory, with twice the energy on impact. Its maximum effective range is over 4,000 m, allowing launch from beyond the envelope of most short-range anti-aircraft weapons. In comparison, the Mighty Mouse or Hydra 70 requires launches from much shorter ranges, potentially placing the launch aircraft within the range of ground-based weapons arranged around the target.
Unguided rockets are normally spin stabilized like rifle bullets. The spin is imparted by small fins at the rear of the rocket body that flip out into the airstream once the rocket leaves its launch tube. The fins take a short time to open and more time to start the rocket spinning. During this period, the rockets can drift significantly from their original aim point. The CRV7 solved this problem by adding small vanes projecting into the rocket exhaust to start the rocket spinning even before it left the launch tube, greatly increasing accuracy. A salvo of CRV7's will impact the target area in one-third the footprint of older designs.
The weapon was originally quoted to have a dispersion of 4 milliradians, but testing with the McDonnell Douglas CF-18 Hornet demonstrated it was even lower, at 3 milliradians. This is considerably better than the autocannon that arm most aircraft; the widely used 20mm M61 Vulcan is rated at 8 milliradians, while the much larger and considerably heavier 30mm GAU-8 Avenger is rated at 5 milliradians.
The CRV7 had just been introduced into Royal Canadian Air Force service when it was entered as a part of a general competition in France. One part of the competition required the contestants to hit a tower with unarmed rockets. The Canadian pilot hit it on his first try, but aimed as if firing the much lower-powered Mk 40 and was therefore close enough that the rocket motor was still firing. The remaining unburned propellant shattered, allowing more surface area of the rocket motor to burn, in turn increasing the pressure and rate of combustion until it became a deflagration that destroyed the tower. The pilot was disqualified because the judges refused to believe it was unarmed.
The aluminium-based fuel in the C-14 engine generated considerable amounts of smoke. While suitable for high-speed aircraft that quickly clear the plume, it is not suitable for slower aircraft and helicopters which would be flying in the smoke for some period of time. This problem led to the development of the RLU-5002/B (C-15) engine, which did not include aluminium and produced considerably less smoke, with a slightly lower impulse of 2,185 lbf·s (9.7 kN·s). The original C-15 used a tail-mounted igniter that was ejected by the rocket when it was fired. In some cases the igniter would hit the aircraft, causing minor damage. To address this, the RLU-5002A/B (HEPI) was introduced, with a "Head-End Permanent Igniter" that is not ejected on launch.
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CRV7
The CRV7, short for "Canadian Rocket Vehicle 7", is a 2.75-inch (70 mm) folding-fin ground attack rocket produced by Bristol Aerospace in Winnipeg, Manitoba. It was introduced in the early 1970s as an upgraded version of the standard U.S. 2.75-inch air-to-ground rocket. It was the most powerful weapon of its class, the first with enough energy to penetrate standard Warsaw Pact aircraft hangars. The CRV7 remains one of the most powerful air-to-ground attack rockets to this day, and has slowly become the de facto standard for Western-aligned forces outside the United States. Beginning in 2021, 83,303 stored Canadian CRV7s are slated for disposal, having been removed from service from 2005 to 2007. In 2024 the Department of National Defence was considering donating the rockets to Ukraine as military aid to defend against the Russian invasion of Ukraine. An estimated 8,000 rockets have functioning warheads, while the remainder could be used for parts or modification. In September 2024 Canadian defence minister Bill Blair announced Canada would be sending 80,840 rocket motors to Ukraine over the next months, in addition to the 2,100 already shipped, along with 1,300 warheads.
The CRV7 was an offshoot of late 1950s research at CARDE (now DRDC Valcartier) into high-performance solid fuel rockets, research performed as a part of a general program studying anti-ballistic missiles. With Aerojet's assistance, CARDE and Bristol developed the "Propulsion Test Vehicle" to test new fuel and engine designs. This program led to the development of the Black Brant sounding rocket, which first flew in 1960 and has had a long and successful career since then. Engineer Jose Tharayil from Bristol Aerospace is considered the driving force behind the CRV7's development and production.
In the early 1970s, CARDE and Bristol decided to use the same propellant and engine design for a new 2.75-inch rocket to equip the Canadair CF-104 Starfighter. The resulting RLU-5001/B (C-14) engine was first delivered by Bristol in production form in 1973. It had a total impulse of 2,320 lbf·s (10.3 kN·s) and a burn time of 2.2 seconds. The empty weight of the rocket is 6.6 kg, and it is normally equipped with a 10 lb (4.5 kg) high-explosive warhead taken from U.S. rockets.
Compared to the U.S. Mk 40 FFAR Mighty Mouse rockets the CRV7 replaced, the higher energy fuel and newer fuselage design led to a longer and much flatter trajectory, with twice the energy on impact. Its maximum effective range is over 4,000 m, allowing launch from beyond the envelope of most short-range anti-aircraft weapons. In comparison, the Mighty Mouse or Hydra 70 requires launches from much shorter ranges, potentially placing the launch aircraft within the range of ground-based weapons arranged around the target.
Unguided rockets are normally spin stabilized like rifle bullets. The spin is imparted by small fins at the rear of the rocket body that flip out into the airstream once the rocket leaves its launch tube. The fins take a short time to open and more time to start the rocket spinning. During this period, the rockets can drift significantly from their original aim point. The CRV7 solved this problem by adding small vanes projecting into the rocket exhaust to start the rocket spinning even before it left the launch tube, greatly increasing accuracy. A salvo of CRV7's will impact the target area in one-third the footprint of older designs.
The weapon was originally quoted to have a dispersion of 4 milliradians, but testing with the McDonnell Douglas CF-18 Hornet demonstrated it was even lower, at 3 milliradians. This is considerably better than the autocannon that arm most aircraft; the widely used 20mm M61 Vulcan is rated at 8 milliradians, while the much larger and considerably heavier 30mm GAU-8 Avenger is rated at 5 milliradians.
The CRV7 had just been introduced into Royal Canadian Air Force service when it was entered as a part of a general competition in France. One part of the competition required the contestants to hit a tower with unarmed rockets. The Canadian pilot hit it on his first try, but aimed as if firing the much lower-powered Mk 40 and was therefore close enough that the rocket motor was still firing. The remaining unburned propellant shattered, allowing more surface area of the rocket motor to burn, in turn increasing the pressure and rate of combustion until it became a deflagration that destroyed the tower. The pilot was disqualified because the judges refused to believe it was unarmed.
The aluminium-based fuel in the C-14 engine generated considerable amounts of smoke. While suitable for high-speed aircraft that quickly clear the plume, it is not suitable for slower aircraft and helicopters which would be flying in the smoke for some period of time. This problem led to the development of the RLU-5002/B (C-15) engine, which did not include aluminium and produced considerably less smoke, with a slightly lower impulse of 2,185 lbf·s (9.7 kN·s). The original C-15 used a tail-mounted igniter that was ejected by the rocket when it was fired. In some cases the igniter would hit the aircraft, causing minor damage. To address this, the RLU-5002A/B (HEPI) was introduced, with a "Head-End Permanent Igniter" that is not ejected on launch.
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