Lockheed D-21B (#537)  Drone


Description
Manufacturer: Lockheed
Designation: D-21
Version:  B
Nickname:  
Type: Reconnaissance
Specifications (Lockheed D-21A)
Length:  42 ft  10 in   M
Height:     M
Wingspan:  19 ft  M
    lbs  Kg
Launch Weight: 11,000  lbs  Kg
Propulsion
No. of Engines: 1
Powerplant:  Marquardt ramjet RJ43-MA-11 using JP-7 fuel
Thrust (each):
Performance
Range: 3,450 miles   Km
Max Speed:  2,700 Mph   Km/H  Kt
Ceiling:  95,000 Ft   M


Lockheed D-21 Drone

 The Lockheed D-21 was a Mach 3+ reconnaissance drone. The drone was originally designed to be launched off the back of its A-12-based M-21 aircraft. Development began in October 1962. Originally known by the Lockheed designation Q-12, it was intended for reconnaissance missions deep into enemy airspace. The D-21 was designed to carry a single high-resolution photographic camera over a pre-programmed path, then release the camera module into the air for retrieval and self-destruct.  

In late 1963, the project was named "Tagboard"; the Q-12 was re-designated D-21 while the A-12 version became M-21 (D- for "daughter" and M- for "mother"). Two production slots from the original 18 A-12 units were designated for the M-21, serial numbers 60-6940, and -6941. The M-21 was a two-seat version of the A-12, with a pylon on the fuselage centerline between the tailfins to carry the drone in a nose-up attitude. A periscope allowed the back-seater, or "Launch Control Operator (LCO)", to observe the D-21. Two M-21s were built, along with an initial batch of seven D-21s for test flights.

The M-21/D-21 program was canceled after an in-flight accident in July 1966. After this the D-21 drone was modified to the D-21B version to add a booster rocket and mount on an underwing pylon on B-52Hs. After flight testing and four operational launches, the B-52H/D-21B program was ended in July 1971.

The D-21 Drone was delivered to the museum on July 19, 2007, and it is on loan from the USAF.

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