About: McDonnell Douglas F-15 STOL/MTD   Sponge Permalink

An Entity of Type : dbkwik:resource/AGhloO_nVTaFp7GvOmHv5Q==, within Data Space : 134.155.108.49:8890 associated with source dataset(s)

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 to 2008. With the help of thrust vectoring nozzles, this aircraft can perform the famous Pugachev's Cobra maneuver. While with NASA, the plane's tail number was 837; for the Quiet Spike program and Research Testbed it was 836, and 835 was used for the Highly Integrated Digital Electronic Control (HIDEC) program.

AttributesValues
rdf:type
rdfs:label
  • McDonnell Douglas F-15 STOL/MTD
rdfs:comment
  • 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 to 2008. With the help of thrust vectoring nozzles, this aircraft can perform the famous Pugachev's Cobra maneuver. While with NASA, the plane's tail number was 837; for the Quiet Spike program and Research Testbed it was 836, and 835 was used for the Highly Integrated Digital Electronic Control (HIDEC) program.
sameAs
dcterms:subject
dbkwik:nasa/proper...iPageUsesTemplate
max takeoff weight alt
  • 31930.0
loaded weight main
  • 44442.0
  • 47000.0
max speed more
  • at
length alt
  • 19.42 m
  • 19.7 m
span main
  • 42.8
lists
  • *List of experimental aircraft *List of military aircraft of the United States
thrust alt
  • 63.88 kN
  • 79 kN
height alt
  • 5.64 m
primary user
  • United States Air Force
Type
  • Technology Demonstrator and Research Aircraft
range alt
  • 4405.0
length main
  • 63(xsd:double)
  • 64.0
area main
  • 608.0
  • 626.0
height main
  • 563.88
span alt
  • 13 m
payload alt
  • 7112.0
range main
  • 2737.0
Manufacturer
  • McDonnell Douglas
max speed main
  • Mach 2.0
  • Mach 2.1
ceiling main
  • 60000.0
  • 58220.0
afterburning thrust main
  • 23780(xsd:integer)
  • 29000.0
National Origin
  • United States
empty weight main
  • 26966.0
  • 35000.0
Related
  • *F-15 Eagle *F-15E Strike Eagle
afterburning thrust alt
  • 105.78 kN
  • 129 kN
type of jet
  • turbofan engines, equipped with Pratt & Whitney P/YBBN 20 Degree three-dimensional thrust vectoring nozzles
  • turbofan engines, equipped with Pratt & Whitney 20 Degree two-dimensional thrust vectoring nozzles, reverse thrust capable
loaded weight alt
  • 20159.0
  • 21319.0
Developed From
area alt
  • 56.5
  • 58.2
First Flight
  • 1988-09-07(xsd:date)
more users
engine (jet)
  • Pratt & Whitney F100-PW-100
  • Pratt & Whitney F100-PW-229
max speed alt
  • 1522(xsd:integer)
  • 1650(xsd:integer)
jet or prop?
  • jet
empty weight alt
  • 12232.0
  • 15876.0
thrust main
  • 14360(xsd:integer)
  • 17800(xsd:integer)
number of jets
  • 2(xsd:integer)
plane or copter?
  • plane
ceiling alt
  • 17,750 m
  • 18,288 m
similar aircraft
  • *Rockwell-MBB X-31 *Sukhoi Su-37
max takeoff weight main
  • 70400.0
variants with their own articles
Retired
  • 1991-08-15(xsd:date)
  • 2009-01-30(xsd:date)
payload main
  • 17000.0
Crew
  • Two
  • two
Number Built
  • 1(xsd:integer)
ref
  • NASA.
more general
  • *Fuel capacity: 11,520 lb *Horizontal tail span: 28.2 ft *Canard span: 25.6 ft
abstract
  • 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 to 2008. With the help of thrust vectoring nozzles, this aircraft can perform the famous Pugachev's Cobra maneuver. While with NASA, the plane's tail number was 837; for the Quiet Spike program and Research Testbed it was 836, and 835 was used for the Highly Integrated Digital Electronic Control (HIDEC) program.
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