87606039 aircraft line drawings
DESCRIPTION
Aircraft line drawingsTRANSCRIPT
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Centurion (front)
Centurion (side)
Centurion (top)
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35
40
300"143.6"
49
98"
504"
Maximum diameter = 60"Forward staticpressure orifices
57"
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Free floating slat
D-558-IIwing configurations
Wing-fenceBasic wing Wing-fence (2) Wing-fence/slat
Fixed slat Leading-edgechord extension
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Wingtip accelerometers
Leading edge flap control
Push-pull tubes longitudinal control
Aircraft pitch rate gyros
Aircraft normal accelerometers
Wingtip accelerometers
First sym W/B bending 4 Hz
Stabilon surface
First sym bending 12.8 Hz
Control sticksPitch damperPitch stick transducersPitch feel springSeries trim actuator
M
Trailing edge flap control
M
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42.83
18.67 ft
63.75 ft
837
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54.2 ft
17.7 ft
32.5 ft
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840
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845
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845
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804
NASA
NOR THR OP
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HL-10 HL-10 modified
Separated flow Attached flow
Cambered leading edge
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NORTHROP
RESCUE
804
NASA
BEWARE OF BLAST
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Wing flap Rudder
Top hatch
Body flaps
Body flaps
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Helios (front)
Helios (side)
247'Helios (top)
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LoFLYTE Aircraft Configuration
Top view
Side viewFront view
Length: 8 ft 4 in.
Weight: 70 lbs
Performance: Maximum speed 240 knots
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NACA
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NAC
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803NASA
NOR THR OP
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III
III
CBA EC
14
3
5
26
711
10
9
8
14
16
17
18
13
1215
20
19
21 24
25
22
2327
26
29
2830
31
Identification Key for :
"Celebrating One Hundred Years of Powered Flight 1903-2003" by Dr. Robert T. McCall 2003
Medium: oil on canvas Dimensions: 6 feet by 18 feet Commissioned by NASA Dryden Flight Research Center, Edwards, CA.
Central Quote:"It is my belief that flight is possible..." Wilbur Wright September 3rd, 1900From a letter written to his father, announcing his intention to make "some experiments with a flying machine" at Kitty Hawk, North Carolina.
Numbering sequence: left to right, top to bottomPeopleA. U.S. World War I Aviator D. NASA Shuttle AstronautB. U.S. World War II Flier E. Space WalkersC. NASA Research PilotPlanetsI. Saturn III. MarsII. Moon IV. Jupiter
Aircraft and Spacecraft (Numbered 1-31) 1. Wright EX "Vin Fiz" 2. Curtiss Model D Headless Pusher 3. Curtiss June Bug 4. Wright 1909 Military Flyer
6. Curtiss 1911 Model D 7. Douglas World Cruiser (DWC) (formation) 8. Ryan NYP "Spirit of St. Louis" 9. North American P-51D Mustang (formation)10. Boeing B-17 Flying Fortress 11. Douglas SBD Dauntless (formation)
5. Bleriot XI
16. Lockheed SR-71A Blackbird17. North American X-1518. Bell X-1 "Glamorous Glennis"19. Boeing 747-100 NASA Shuttle Carrier Aircraft (SCA) Shuttle Orbiter Enterprise (OV-101)
12. Boeing Model 314 Clipper13. Consolidated PBY Catalina14. Boeing B-29 Superfortress (Navy P2B-1S)/Douglas D-558-2 Skyrocket (launch)15. Douglas DC-3
22. Boeing 77723. Lockheed F-117 Nighthawk "Stealth Fighter"24. Rutan Model 76 Voyager
20. Wright 1903 Flyer21. Douglas D-558-2 Skyrocket
25. Grumman F-14 Tomcat (formation)26. Bell UH-1 Iroquois (Huey)27. Apollo Spacecraft/Saturn V Launch Vehicle28. Grumman Lunar Module (LM)29. Rockwell Shuttle (Space Transportation System)30. International Space Station31. Rockwell Space Shuttle OrbiterNaming and Designation Source: Directory of Airplanes, their Designers and Manufacturers Edited by Dana Bell, copyright 2002 The Smithsonian National Air and Space Museum ISBN 1-85367-490-7
Key created by NASA Dryden Graphics Dept.
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2.50
107.40
41.21
Model
SR-71/LASRE ConfigurationNote:All dimensions in feet
18.50
7.531.86 Canoe
Reflector plane
2.75
55.60 55.60
7.50
17.32
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U S A
United States
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USA Challenger
United States
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S A
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Ball nose config.
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U.S. AIR FORCE
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NACA
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Time
Altitude
B-52 with Lifting Bodyattached to pylon under wing
Lifting Body launchedfrom B-52
Maximum missionaltitude attained;
rocket engine shutdown
Unpowered steepglide to lakebed
landing
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14 ft 9.5 in.
Strake flap
Canard
Wing flap
48 ft 1 in.
27 ft 2.44 in.
F-5A nosesection
Rudder
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EFMX-31
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Normal Bell-NozzleRocket Engine
Linear AerospikeRocket Engine
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58.3 ft
27.7 ft
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ConventionalJet Engine
Scramjet EngineSupersonic combustion ramjets, or Scramjets,operate by burning fuel in a stream ofsupersonic air compressed by theforward speed of the aircraft.Unlike conventional jet engines,scramjets have no rotating parts.In normal jet engines, rotatingblades compress the air,and the airflow remainssub-sonic.
The supersonic airflow intothe engine is compressedmore as it enters the inletand passes through theengine. This increases theair pressure higher thanthe surrounding air.
Hydrogen fuel is ignitedin the supersonic airflow,with the rapid expansionof hot air out the exhaustnozzle producing thrust.
Rotating compressor blades draw in air and compress it.Mixture of fuel and air burns and expands in combustion chamber.
Hot, compressed air is forced out the exhaust nozzle, producing thrust.
X-43
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5 ft
12 ft
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Hyper-X
Pegasus booster
Interstage adapter
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105 f(32m)
Ground line185.75 ft(56.62m)
30 ft(9.1m
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