F-15 S/MTD / F-15 ACTIVE
Role	Technology Demonstrator and Research Aircraft
National origin	United States
Manufacturer	McDonnell Douglas
First flight	September 7, 1988
Retired	August 12, 1991
Primary users	United States Air Force NASA
Number built	1
Developed from	F-15 Eagle
Variants	F-15 Intelligent Flight Control System

The McDonnell Douglas F-15 S/MTD (Short Takeoff and Landing/Maneuver Technology Demonstrator) is a modified F-15 Eagle. Developed as a technology demonstrator, the F-15 S/MTD carried out research for studying the effects of vectored thrust and enhanced maneuverability. The aircraft used for the project was pre-production TF-15A (F-15B) #1 (USAF S/N 71-0290), the first delivered F-15 airframe, which is on loan to NASA from the United States Air Force.

This same aircraft would later be used in the F-15 ACTIVE (Advanced Control Technology for Integrated Vehicles) from 1993–1999, and later in the Intelligent Flight Control System programs from 1999 on. With the help of thrust vectoring nozzles, this aircraft can perform the famous Pugachev's Cobra maneuver.

Contents 1 Design and development 1.1 F-15 S/MTD special features 1.2 Further modifications 2 Specifications 2.1 F-15 S/MTD 2.2 F-15 ACTIVE 3 See also 4 References 5 External links

[edit] Design and development

The aircraft used in the S/MTD program has flown several times since the successful S/MTD program completion in 1991 that used vectored thrust and canard foreplanes to improve low-speed performance. This aircraft tested high-tech methods for operating from a short runway. This F-15 was part of an effort to improve ABO (Air Base Operability), the survival of warplanes and fighting capability at airfields under attack.

The F-15 S/MTD tested ways to land and take off from wet, bomb-damaged runways. The aircraft used a combination of reversible engine thrust, jet nozzles that could be deflected by 20 degrees, and canard foreplanes. Pitch vectoring/reversing nozzles and canard foreplanes were fitted to the F-15 in 1988. NASA acquired the plane in 1993 and replaced the engines with Pratt & Whitney F100-229 engines with Pitch/Yaw vectoring nozzles. ^[1] The canard foreplanes were derived from the F/A-18's stabilator.

Prior to 1991, when McDonnell Douglas ended its program after accomplishing their flight objectives, the F-15 STOL/MTD plane achieved some impressive performance results:^[2]

• demonstrated vectored takeoffs with rotation at speeds as low as 42 mph (68 km/h)
• a 25-percent reduction in takeoff roll
• landing on just 1,650 ft (500 m) of runway compared to 7,500 ft (2,300 m) for the standard F-15
• thrust reversal in flight to produce rapid decelerations
• controlled flight at angles of attack up to about 85 deg without vertical-tail surfaces

[edit] F-15 S/MTD special features

• Canards Foreplanes: The canards fitted to the front of the aircraft improve maneuverability in the vertical plane (pitching) by "lifting up the front of the plane", rather than "pushing down the rear". Also, at large angles of attack, they act as airbrakes.
• Thrust-Vectoring Nozzles: By using a combination of the movable nozzles and vanes in the jet pipe, the S/MTD can direct exhaust forward, outward or at an angle of up to 20 degrees to the axis of the aircraft.
• Combined Canard, Elevator and Nozzle effect: With its highly advanced flight control software, the S/MTD coordinates the movement of the forward canards to give up-force, and the tailplanes and nozzles produce a down-force when maneuvering. This produces a pitching moment larger than that possible with the conventional elevator-only configuration. As a result, maneuverability is far improved.
• Fast Stop-Start: By vectoring engine exhaust from above and below the nozzles and turning the canard foreplanes to act as giant airbrakes, the S/MTD could decelerate very rapidly and then accelerate fast using its powerful F100 engines. This kind of maneuver might be useful in a dogfight.

[edit] Further modifications

During the 1990s the same F-15 airframe was further modified (canards and nozzles were retained) for the ACTIVE (Advanced Control Technology for Integrated VEhicles) program in which pitch/yaw thrust-vectoring nozzles and advanced control-logic programming were investigated. In the ACTIVE configuration it was also used for the LANCETS (lift and nozzle change effects on tail shock) program, in which computed supersonic shockwave parameters were compared to those measured in flight. The LANCETS flight tests ended in December 2008.^[3] F-15 ACTIVE lasted from 1993–1999.

The aircraft would later be used in the F-15 IFCS (Intelligent Flight Control System) program from 1999.

[edit] Specifications

[edit] F-15 S/MTD

General characteristics

• Crew: Two
• Length: 64 ft (19.7 m)
• Wingspan: 42.8 ft (13 m)
• Height: 18 ft 6 in (5.64 m)
• Wing area: 626 ft² (58.2 m²)
• Empty weight: 26,966 lb (12,232 kg)
• Loaded weight: 44,442 lb (20,159 kg)
• Max takeoff weight: 70,400 lb (31,930 kg)
• Powerplant: 2× Pratt & Whitney F100-PW-200 turbofan engines, equipped with Pratt & Whitney 20 Degree two-dimensional thrust vectoring nozzles, reverse thrust capable
  • Dry thrust: 14,360 lbf (63.88 kN) each
  • Thrust with afterburner: 23,780 lbf (105.78 kN) each

Performance

• Maximum speed: Mach 2.1 at 37,650 ft (11,480 m) (1,650 mph, 2,650 km/h at 11,500 m)
• Range: 2,737 mi (4,405 km)
• Service ceiling: 58,220 ft (17,750 m)

[edit] F-15 ACTIVE

General characteristics

• Crew: two
• Payload: 17,000 lb (7,112 kg)
• Length: 63.7 ft excluding flight test nose boom (19.42 m)
• Wingspan: 42.8 ft (13 m)
• Height: 18 ft 6 in (5.64 m)
• Wing area: 608 ft² (56.5 m²)
• Empty weight: 35,000 lb (15,876 kg)
• Loaded weight: 47,000 lb (21,319 kg)
• Powerplant: 2× Pratt & Whitney F100-PW-229 turbofan engines, equipped with Pratt & Whitney P/YBBN 20 Degree three-dimensional thrust vectoring nozzles
  • Dry thrust: 23,450 lbf (104 kN) each
  • Thrust with afterburner: 29,000 lb (129 kN) each
• * Fuel capacity: 11,520 lb (5,225 kg) (approx. 1,700 gal)
• Horizontal tail span: 28.2 ft (8.60 m)
• Canard span: 25.6 ft (7.80 m)

Performance

• Maximum speed: Mach 2.5 (1,316 mph, 2,645 km/h)
• Service ceiling: 60,000 ft (18,288 m)

[edit] See also

Related development

• F-15 Eagle
• F-15E Strike Eagle
  

Comparable aircraft

• Sukhoi Su-30
• Sukhoi Su-35
• Sukhoi Su-37
• Mikoyan MiG-35
  

Related lists

• List of fighter aircraft
• List of military aircraft of the United States
  

[edit] References

• Aircraft of the World: The Complete Guide.

[edit] External links

Wikimedia Commons has media related to: F-15S/MTD

• NASA Dryden Fact Sheet - F-15 ACTIVE

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