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BGM-34B ATTACK & MULTI-MISSION RPV

The AUVM founder, LT COL HAROLD (RED) F. SMITH, acquired the drone approximately 30 years ago. The drone has been pulled out of storage and we have began the restoration process.  We are in the mock up phase of the restoration, and it's a bit painstaking as we currently are lacking manuals. We will update the Facebook page and our website as progress is made. 

 

"In the late 1960s, the Navy studied the possibility to convert the BQM-34A Firebee target drone to a remote-controlled anti-ship missile. In several test flights, BQM-34As equipped with a TV system in the nose, were successfully flown by remote "pilots" watching the TV image. Precision low-level flight above the sea was made possible by the Ryan-developed RALACS (Radar Altimeter Low Altitude Control System). In September 1971, successful tests of Model 248 missiles (called "BQM/SSM") against ship targets showed the validity of the basic concept, but the project was terminated due to lack of funding."

"In the same year, the USAF showed interest in a development of the Firebee I to be used for enemy air-defense suppression, because of the high loss rate in these missions. In March 1971, Teledyne Ryan received a contract to convert four Model 147S drones to BGM-34A (Model 234) configuration. Like the Navy's BQM/SSM, the BGM-34A was piloted by an operator watching a TV image transmitted from the drone's nose. In tests during 1971/72, the BGM-34As successfully launched AGM-65 Maverick air-to-surface missiles and electro-optically guided glide bombs against simulated SAM sites. Interestingly, almost 30 years later a firing of an AGM-114 Hellfire missile by an MQ-1L Predator UAV was much hyped as a breakthrough in armed UAV technology. "

Following the successful BGM-34A tests, Teledyne Ryan developed the BGM-34B (Model 234A) operational strike RPV. This featured the higher-rated J69-T-41A engine, a modified tail, larger control surfaces, and improved operational capabilities. Eight BGM-34Bs were built, and tested in 1973/74. The tests included the modification of some of the drones with a new nose containing a LLLTV (Low Light Level Television) camera and a laser designator, to act as a "pathfinder" for weapon-carrying RPVs." 

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Radioplane OQ-2

The OQ-2 is a simple aircraft, powered by a two-cylinder two-cycle piston engine, providing 6 horsepower (4.5 kW) and driving two contra-rotating propellers. The RC control system was built by Bendix.

Launching was by catapult only and recovered by parachute should it survive the target practice. The landing gear was used only on the OQ-2 versions as sold to the Army to cushion the landing by parachute.

None of the drones including the improved variants shipped to the Navy had landing gear. The subsequent variants delivered to the Army did not have landing gear.


 

The OQ-2 led to a series of similar but improved variants, with the OQ-3 / TDD-2 and OQ-14 / TDD-3 produced in quantity. During the war Radioplane manufactured nearly fifteen thousand drones. The company was bought by Northrop in 1952.

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Northrop BQM/MQM-74 “Chukar”

The BQM/MQM-74 “Chukar” is a series of aerial target drones produced by Northrop. It is a recoverable, remote controlled, subsonic aerial target drone, capable of speeds up to Mach 0.86 and altitudes from 30 feet to 40,000 feet.

It was introduced in 1968 and many are still in service.  It is normally launched from a DC-130 aircraft, but can also be launched from strike fighters such as the F-15 and F-16 as well as from ships.


 

In the 1991 Gulf War, BQM-74Cs were used as decoys during the initial air attacks into Iraq. When Iraqi air defense radar sites began tracking them, allied strike fighters were then able to launch anti-radiation missiles to destroy the sites. The U.S. Air Force was put in charge of this multi-service decoy effort, which was codenamed “Project Scathe Mean.”


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MQM-57 Falconer

Surveillance Drone 1 or SD-1—originally was a target for training anti-aircraft gunners.  The MQM-57 became the Army's 1st unmanned reconnaissance aircraft, Equipped with still picture and TV cameras in 1955! The drone was launched off of a take off stand with two RATO Boosters. A remote pilot controlled the Falconer with radio signals and tracked by radar. 

Crew: 0

Length: 13, 4"

Wingspan: 11' 6"

Weight: 430 LBS

Service Ceiling: 15,000'

Max Speed: 184  MPH

Range: 100 Miles

Flight Time: 30-60 MINS



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QH-50 Gyrodyne- DASH "Lucy"

 DASH was a major part of the United States Navy's Fleet Rehabilitation and Modernization (FRAM) program of the late 1950s.

FRAM was started because the Soviet Union was building submarines faster than the US could build anti-submarine frigates. Instead of building frigates, the FRAM upgrade series allowed the US to rapidly update by converting older ships that were less useful in modern naval combat. The navy could upgrade the sonar on World War II-era destroyers but needed a stand-off weapon to attack at the perimeter of the sonar's range. The old destroyers had little room for add-ons such as a full flight deck.

The original DASH concept was a light drone helicopter that could release a nuclear depth charge or torpedoes. The aircraft was considered expendable. 


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Culver PQ-14 Cadet

In 1940, before the Air Force, The US Army Crops desired a radio controlled target drone for anti-aircraft gunnery practice. The aircraft was unique as it was both manned, and unmanned operated.

 

Length: 19,6"

Wingspan: 30'

Height: 8'4

Powerplant: Franklin 6cyl, 150 HP

Max Speed: 185 MPH

Cruise Speed: 150 MPH

Range: 512 Miles

 

The Culver was first flown in 1942! The drone was flown unamnned, by radio control via mothership, Beech C-45. Most drones were destroyed in the Sky by anti-aircraft gunners, but a few survived included this one. It will under go restoration.

 

The bird has been in storage for 40 YEARS! We just got it mock assembled and rolling on it's landing gear!



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Lockheed X7-A

Lockheed X7-A "Flying Stove Pipe" was designed to test Ram Jet engines & our air defenses against nuclear missile attack. The drone was tested against our SAM's, and the X7 outperformed the missiles and only a few hits were achieved; Due to the pressure and embarrassment put on the military, the X7 project was trashed. Besides the SAM testing, the X-7 was also used to test communication equipment, testing aerodynamics, thermodynamics, parachute systems, and booster propellants.

 

Specs:

Length: 32'9"

Wingspan: 12'

Height: 7'

Weight: 8,000 lbs

Speed: 2800 MPH

Ceiling: 100,000'

Range: 130 Miles

Booster: X202 C3 Solid Rocket Fuel, 467 kN for approx 4 seconds.

 

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