History of Interstate Aircraft TDR
One of the US military's earliest forays into unmanned attack drone aircraft was the World War II era Interstate Aircraft and Engineering Corporation (IAEC) "TDR" (1939-1945). The main driving force behind its development was the fierce struggle of the United States Navy (USN) against the power of the Japanese Empire.
The aircraft first flew in 1942, at a time when U.S. involvement in the war was increasingthough it didn't officially enter production until September 1944. The aircraft was actively used by the U.S. military against the Japanese in the Pacific, but technical problems and proven conventional solutions ultimately thwarted this novel, forward-looking projectits last days of flight were recorded in October 1944 .
In addition to being used by the USN, the U.S. Army Air Forces (USAAF) considered the TDR program enough to retain several names - the industry has only seen a few prototypes emerge. The concept of the long-range attack aircraft was pioneered by Lieutenant Colonel D.S. Farney and accelerated the development of advanced technology in the shadow of World War I. In April 1942, as the United States was already committed to war in Africa, Europe, and the Pacific, the U.S.
Navy recorded its first successful drone test-fire attack.
Interstate Aircraft, a pre-war airline founded in 1937, was awarded a development contract to continue this work. By 1942, the company had only the S-1 "Cadet", a light, purpose-built high-wing monoplane (though 574 were built for service with the US Air Force).
The company received funding for two prototypes and 100 follow-on carrier-grade production aircraft, which fall under the "TDR" designation.
The original experimental prototype was aptly named "XTDR-1". Work on these airframes culminated in the final production form of the "TDR-1", of which 189 were built to the XTDR-1 prototype standard.
In the TDR arrangement, the aircraft will be flown by specially modified TV-equipped Grumman TBF "Avengers" Navy dive bombers, relying on "novelty" technologies such as radar altimeters and long-range cameras/original forms of communication. From the exterior From the above, the shape of this aircraft is very traditional, with a slender fuselage, a low-mounted monoplane main aircraft, and a monoplane tail.
A disposable tricycle landing gear helps guide the plane over the ground. Inside, a tubular steel structure supports the fuselage, and a sparse molded veneer covers the entire assembly.
When complete, the TDR has a wingspan of 48 feet and a total weight of 5,900 pounds. The twin-engine arrangement is powered by 2 Lycoming O-435-2 opposed-piston engines, each delivering up to 220 hp, while the twin-blade propellers rotate in a trailer configuration.
The engines are located in the nacelles on the leading edge of the main fuselage of each wing.
Specification
Basics
Year of Service
1942
Origins
United States
Status
retirement
does not work.
Crew
0
Production
195
Manufacturer
Interstate Aircraft and Engineering Corporation - USA
Operators
United States
Roles
Ground attack (bombing, strafing)
The ability to conduct air strikes against ground targets using (but not limited to) artillery, bombs, rockets, rockets, etc.
Disable support (CAS)
Designed to operate near active ground elements with a wide range of air-to-surface weapon and ammunition options.
Special Mission: Anti-ship
Equipped to find, track, and attack enemy surface elements through visual acquisition, radar support, and ship-based weapons.
nautical/navy
Water mobility capability for a variety of land-based or ship-based maritime missions, supported by Allied Naval Surface Forces.
Intelligence Surveillance Reconnaissance (ISR), reconnaissance
Monitor ground targets/target areas to assess surrounding threat levels, enemy strength, or enemy movement.
X-Plane (development, prototype, tech demo)
Aircraft designed for prototyping, technology demonstration, or research/data collection.
Unmanned ability
Aircraft designed (or later developed) have inherent unmanned capabilities and can fill a variety of battlefield roles.
Notable Features
Extended Range Performance
Ability to travel long distances using on-board fuel supplies.
Operation Lakes
Able to operate over the ocean and survive certain harsh marine environments.
torpedo weapons
Ability to launch/release torpedoes against maritime threats/targets.
Unmanned operation
The design features the ability to fly without a pilot, with actions controlled by onboard programming and/or ground operators.
Dimensions and Weights
Width/Span
49. 2 feet
(15.00m)
Cured weight
5,897 lbs
(2,675 kg)
MTOW
7,937 lbs
(3,600 kg)
Wgt Difference
+?2,039
(+925kg)
MAINPLANE STRUCTURE
wing/low/straight
Monoplane
Designed to use a single main wing main aircraft; this is the most popular arrangement of main aircraft.
install low
The main aircraft is mounted low on the side of the fuselage.
Straight
Floor plans involve the use of simple, straight main plan elements.
(Structure descriptor reference production variant Interstate TDR-1)
Performance
Installed:
2 x Lycoming O-435-2 220 hp opposed-piston engines, each driving a two-bladed propeller unit.
Maximum speed
155 km/h
(250 km/h | 135 kn)
Cruising speed
143 km/h
(230 km/h | 124 knots)
Maximum speed difference
+12 km/h
(+20 km/h | 11 kn)
Maximum
6,004 feet
(1,830 m | 1 mile)
Area
426 km
(685 km | 1,269 nautical miles)
Range (MPH) Subsonic: <614mph | Transonic: 614-921 | Supersonic: 921-3836 | Hypersonic: 3836-7673 | Hypersonic: 7673-19180 | Reentry: > 19030
Weapon
1 x 2,000 lb conventionally thrown bomb or aerial torpedo fixed ventral to fuselage centerline. The smaller diameter drops bombs under the wing roots (three hardpoints including the center).

