Skip to main content

Langley Research Center Media Archive



rss RSS
A B C D E F G H I J K L M remove-circle N O P Q R S T U V W X Y Z
SHOW DETAILS
up-solid down-solid
Prior Page
eye
Title
Date Archived
Creator
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 34

favorite 0

comment 0

NASA Army Boom Strakes
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 72

favorite 0

comment 0

Photographed on 03/21/2003. -- Documentation of research installations on the aircraft. L2003-851: Cirrus SR22X - bulkhead penetration in right firewall for engine sensor wires. L2003-852: Cirrus SR22X - fuel flow meter & manifold pressure transducer mounted on upper right side of engine. L2003-853: Cirrus SR22X - optical RPM sensor inside front engine baffle by alternator pulley & belt. L2003-854: Cirrus SR22X - right wing at wingtip attach point. Forward conduit for wires/pitot-static...
Topics: AIRCRAFT DESIGN. -- AIRCRAFT STRUCTURES., What -- Magnetometer, What -- S 15, What -- Dash
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 45

favorite 1

comment 0

Photographed on 03/21/2003. -- Documentation of research installations on the aircraft. L2003-851: Cirrus SR22X - bulkhead penetration in right firewall for engine sensor wires. L2003-852: Cirrus SR22X - fuel flow meter & manifold pressure transducer mounted on upper right side of engine. L2003-853: Cirrus SR22X - optical RPM sensor inside front engine baffle by alternator pulley & belt. L2003-854: Cirrus SR22X - right wing at wingtip attach point. Forward conduit for wires/pitot-static...
Topics: AIRCRAFT DESIGN. -- AIRCRAFT STRUCTURES., What -- Magnetometer, What -- S 15, What -- Dash
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 77

favorite 0

comment 0

Photographed on 03/21/2003. -- Documentation of research installations on the aircraft. L2003-851: Cirrus SR22X - bulkhead penetration in right firewall for engine sensor wires. L2003-852: Cirrus SR22X - fuel flow meter & manifold pressure transducer mounted on upper right side of engine. L2003-853: Cirrus SR22X - optical RPM sensor inside front engine baffle by alternator pulley & belt. L2003-854: Cirrus SR22X - right wing at wingtip attach point. Forward conduit for wires/pitot-static...
Topics: AIRCRAFT DESIGN. -- AIRCRAFT STRUCTURES., What -- Magnetometer, What -- S 15, What -- Dash
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 34

favorite 0

comment 0

Photographed on 03/21/2003. -- Documentation of research installations on the aircraft. L2003-851: Cirrus SR22X - bulkhead penetration in right firewall for engine sensor wires. L2003-852: Cirrus SR22X - fuel flow meter & manifold pressure transducer mounted on upper right side of engine. L2003-853: Cirrus SR22X - optical RPM sensor inside front engine baffle by alternator pulley & belt. L2003-854: Cirrus SR22X - right wing at wingtip attach point. Forward conduit for wires/pitot-static...
Topics: AIRCRAFT DESIGN. -- AIRCRAFT STRUCTURES., What -- Magnetometer, What -- S 15, What -- Dash
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 32

favorite 0

comment 0

Photographed on 03/21/2003. -- Documentation of research installations on the aircraft. L2003-851: Cirrus SR22X - bulkhead penetration in right firewall for engine sensor wires. L2003-852: Cirrus SR22X - fuel flow meter & manifold pressure transducer mounted on upper right side of engine. L2003-853: Cirrus SR22X - optical RPM sensor inside front engine baffle by alternator pulley & belt. L2003-854: Cirrus SR22X - right wing at wingtip attach point. Forward conduit for wires/pitot-static...
Topics: AIRCRAFT DESIGN. -- AIRCRAFT STRUCTURES., What -- Magnetometer, What -- S 15, What -- Dash
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 62

favorite 0

comment 0

Photographed on 03/21/2003. -- Documentation of research installations on the aircraft. L2003-851: Cirrus SR22X - bulkhead penetration in right firewall for engine sensor wires. L2003-852: Cirrus SR22X - fuel flow meter & manifold pressure transducer mounted on upper right side of engine. L2003-853: Cirrus SR22X - optical RPM sensor inside front engine baffle by alternator pulley & belt. L2003-854: Cirrus SR22X - right wing at wingtip attach point. Forward conduit for wires/pitot-static...
Topics: AIRCRAFT DESIGN. -- AIRCRAFT STRUCTURES., What -- Magnetometer, What -- S 15, What -- Dash
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 32

favorite 0

comment 0

Photographed on 03/21/2003. -- Documentation of research installations on the aircraft. L2003-851: Cirrus SR22X - bulkhead penetration in right firewall for engine sensor wires. L2003-852: Cirrus SR22X - fuel flow meter & manifold pressure transducer mounted on upper right side of engine. L2003-853: Cirrus SR22X - optical RPM sensor inside front engine baffle by alternator pulley & belt. L2003-854: Cirrus SR22X - right wing at wingtip attach point. Forward conduit for wires/pitot-static...
Topics: AIRCRAFT DESIGN. -- AIRCRAFT STRUCTURES., What -- Magnetometer, What -- S 15, What -- Dash
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 36

favorite 0

comment 0

Photographed on 03/21/2003. -- Documentation of research installations on the aircraft. L2003-851: Cirrus SR22X - bulkhead penetration in right firewall for engine sensor wires. L2003-852: Cirrus SR22X - fuel flow meter & manifold pressure transducer mounted on upper right side of engine. L2003-853: Cirrus SR22X - optical RPM sensor inside front engine baffle by alternator pulley & belt. L2003-854: Cirrus SR22X - right wing at wingtip attach point. Forward conduit for wires/pitot-static...
Topics: AIRCRAFT DESIGN. -- AIRCRAFT STRUCTURES., What -- Magnetometer, What -- S 15, What -- Dash
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 31

favorite 0

comment 0

Photographed on 03/21/2003. -- Documentation of research installations on the aircraft. L2003-851: Cirrus SR22X - bulkhead penetration in right firewall for engine sensor wires. L2003-852: Cirrus SR22X - fuel flow meter & manifold pressure transducer mounted on upper right side of engine. L2003-853: Cirrus SR22X - optical RPM sensor inside front engine baffle by alternator pulley & belt. L2003-854: Cirrus SR22X - right wing at wingtip attach point. Forward conduit for wires/pitot-static...
Topics: AIRCRAFT DESIGN. -- AIRCRAFT STRUCTURES., What -- Magnetometer, What -- S 15, What -- Dash
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 42

favorite 0

comment 0

Photographed on 03/21/2003. -- Documentation of research installations on the aircraft. L2003-851: Cirrus SR22X - bulkhead penetration in right firewall for engine sensor wires. L2003-852: Cirrus SR22X - fuel flow meter & manifold pressure transducer mounted on upper right side of engine. L2003-853: Cirrus SR22X - optical RPM sensor inside front engine baffle by alternator pulley & belt. L2003-854: Cirrus SR22X - right wing at wingtip attach point. Forward conduit for wires/pitot-static...
Topics: AIRCRAFT DESIGN. -- AIRCRAFT STRUCTURES., What -- Magnetometer, What -- S 15, What -- Dash
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 30

favorite 0

comment 0

Photographed on 03/21/2003. -- Documentation of research installations on the aircraft. L2003-851: Cirrus SR22X - bulkhead penetration in right firewall for engine sensor wires. L2003-852: Cirrus SR22X - fuel flow meter & manifold pressure transducer mounted on upper right side of engine. L2003-853: Cirrus SR22X - optical RPM sensor inside front engine baffle by alternator pulley & belt. L2003-854: Cirrus SR22X - right wing at wingtip attach point. Forward conduit for wires/pitot-static...
Topics: AIRCRAFT DESIGN. -- AIRCRAFT STRUCTURES., What -- Magnetometer, What -- S 15, What -- Dash
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 36

favorite 0

comment 0

Photographed on 03/21/2003. -- Documentation of research installations on the aircraft. L2003-851: Cirrus SR22X - bulkhead penetration in right firewall for engine sensor wires. L2003-852: Cirrus SR22X - fuel flow meter & manifold pressure transducer mounted on upper right side of engine. L2003-853: Cirrus SR22X - optical RPM sensor inside front engine baffle by alternator pulley & belt. L2003-854: Cirrus SR22X - right wing at wingtip attach point. Forward conduit for wires/pitot-static...
Topics: AIRCRAFT DESIGN. -- AIRCRAFT STRUCTURES., What -- Magnetometer, What -- S 15, What -- Dash
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 45

favorite 0

comment 0

Photographed on 03/21/2003. -- Documentation of research installations on the aircraft. L2003-851: Cirrus SR22X - bulkhead penetration in right firewall for engine sensor wires. L2003-852: Cirrus SR22X - fuel flow meter & manifold pressure transducer mounted on upper right side of engine. L2003-853: Cirrus SR22X - optical RPM sensor inside front engine baffle by alternator pulley & belt. L2003-854: Cirrus SR22X - right wing at wingtip attach point. Forward conduit for wires/pitot-static...
Topics: AIRCRAFT DESIGN. -- AIRCRAFT STRUCTURES., What -- Magnetometer, What -- S 15, What -- Dash
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 40

favorite 0

comment 0

Photographed on 03/21/2003. -- Documentation of research installations on the aircraft. L2003-851: Cirrus SR22X - bulkhead penetration in right firewall for engine sensor wires. L2003-852: Cirrus SR22X - fuel flow meter & manifold pressure transducer mounted on upper right side of engine. L2003-853: Cirrus SR22X - optical RPM sensor inside front engine baffle by alternator pulley & belt. L2003-854: Cirrus SR22X - right wing at wingtip attach point. Forward conduit for wires/pitot-static...
Topics: AIRCRAFT DESIGN. -- AIRCRAFT STRUCTURES., What -- Magnetometer, What -- S 15, What -- Dash
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 38

favorite 0

comment 0

Photographed on 03/21/2003. -- Documentation of research installations on the aircraft. L2003-851: Cirrus SR22X - bulkhead penetration in right firewall for engine sensor wires. L2003-852: Cirrus SR22X - fuel flow meter & manifold pressure transducer mounted on upper right side of engine. L2003-853: Cirrus SR22X - optical RPM sensor inside front engine baffle by alternator pulley & belt. L2003-854: Cirrus SR22X - right wing at wingtip attach point. Forward conduit for wires/pitot-static...
Topics: AIRCRAFT DESIGN. -- AIRCRAFT STRUCTURES., What -- Magnetometer, What -- S 15, What -- Dash
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 35

favorite 0

comment 0

Photographed on 03/21/2003. -- Documentation of research installations on the aircraft. L2003-851: Cirrus SR22X - bulkhead penetration in right firewall for engine sensor wires. L2003-852: Cirrus SR22X - fuel flow meter & manifold pressure transducer mounted on upper right side of engine. L2003-853: Cirrus SR22X - optical RPM sensor inside front engine baffle by alternator pulley & belt. L2003-854: Cirrus SR22X - right wing at wingtip attach point. Forward conduit for wires/pitot-static...
Topics: AIRCRAFT DESIGN. -- AIRCRAFT STRUCTURES., What -- Magnetometer, What -- S 15, What -- Dash
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 61

favorite 0

comment 0

Photographed on 03/21/2003. -- Documentation of research installations on the aircraft. L2003-851: Cirrus SR22X - bulkhead penetration in right firewall for engine sensor wires. L2003-852: Cirrus SR22X - fuel flow meter & manifold pressure transducer mounted on upper right side of engine. L2003-853: Cirrus SR22X - optical RPM sensor inside front engine baffle by alternator pulley & belt. L2003-854: Cirrus SR22X - right wing at wingtip attach point. Forward conduit for wires/pitot-static...
Topics: AIRCRAFT DESIGN. -- AIRCRAFT STRUCTURES., What -- Magnetometer, What -- S 15, What -- Dash
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 25

favorite 0

comment 0

Photographed on 03/21/2003. -- Documentation of research installations on the aircraft. L2003-851: Cirrus SR22X - bulkhead penetration in right firewall for engine sensor wires. L2003-852: Cirrus SR22X - fuel flow meter & manifold pressure transducer mounted on upper right side of engine. L2003-853: Cirrus SR22X - optical RPM sensor inside front engine baffle by alternator pulley & belt. L2003-854: Cirrus SR22X - right wing at wingtip attach point. Forward conduit for wires/pitot-static...
Topics: AIRCRAFT DESIGN. -- AIRCRAFT STRUCTURES., What -- Magnetometer, What -- S 15, What -- Dash
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 30

favorite 0

comment 0

Photographed on 03/21/2003. -- Documentation of research installations on the aircraft. L2003-851: Cirrus SR22X - bulkhead penetration in right firewall for engine sensor wires. L2003-852: Cirrus SR22X - fuel flow meter & manifold pressure transducer mounted on upper right side of engine. L2003-853: Cirrus SR22X - optical RPM sensor inside front engine baffle by alternator pulley & belt. L2003-854: Cirrus SR22X - right wing at wingtip attach point. Forward conduit for wires/pitot-static...
Topics: AIRCRAFT DESIGN. -- AIRCRAFT STRUCTURES., What -- Magnetometer, What -- S 15, What -- Dash
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 41

favorite 0

comment 0

Photographed on 03/21/2003. -- Documentation of research installations on the aircraft. L2003-851: Cirrus SR22X - bulkhead penetration in right firewall for engine sensor wires. L2003-852: Cirrus SR22X - fuel flow meter & manifold pressure transducer mounted on upper right side of engine. L2003-853: Cirrus SR22X - optical RPM sensor inside front engine baffle by alternator pulley & belt. L2003-854: Cirrus SR22X - right wing at wingtip attach point. Forward conduit for wires/pitot-static...
Topics: AIRCRAFT DESIGN. -- AIRCRAFT STRUCTURES., What -- Magnetometer, What -- S 15, What -- Dash
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 27

favorite 0

comment 0

Photographed on 03/21/2003. -- Documentation of research installations on the aircraft. L2003-851: Cirrus SR22X - bulkhead penetration in right firewall for engine sensor wires. L2003-852: Cirrus SR22X - fuel flow meter & manifold pressure transducer mounted on upper right side of engine. L2003-853: Cirrus SR22X - optical RPM sensor inside front engine baffle by alternator pulley & belt. L2003-854: Cirrus SR22X - right wing at wingtip attach point. Forward conduit for wires/pitot-static...
Topics: AIRCRAFT DESIGN. -- AIRCRAFT STRUCTURES., What -- Magnetometer, What -- S 15, What -- Dash
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 51

favorite 0

comment 0

Photographed on 03/21/2003. -- Documentation of research installations on the aircraft. L2003-851: Cirrus SR22X - bulkhead penetration in right firewall for engine sensor wires. L2003-852: Cirrus SR22X - fuel flow meter & manifold pressure transducer mounted on upper right side of engine. L2003-853: Cirrus SR22X - optical RPM sensor inside front engine baffle by alternator pulley & belt. L2003-854: Cirrus SR22X - right wing at wingtip attach point. Forward conduit for wires/pitot-static...
Topics: AIRCRAFT DESIGN. -- AIRCRAFT STRUCTURES., What -- Magnetometer, What -- S 15, What -- Dash
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 35

favorite 0

comment 0

Photographed on 03/21/2003. -- Documentation of research installations on the aircraft. L2003-851: Cirrus SR22X - bulkhead penetration in right firewall for engine sensor wires. L2003-852: Cirrus SR22X - fuel flow meter & manifold pressure transducer mounted on upper right side of engine. L2003-853: Cirrus SR22X - optical RPM sensor inside front engine baffle by alternator pulley & belt. L2003-854: Cirrus SR22X - right wing at wingtip attach point. Forward conduit for wires/pitot-static...
Topics: AIRCRAFT DESIGN. -- AIRCRAFT STRUCTURES., What -- Magnetometer, What -- S 15, What -- Dash
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 26

favorite 0

comment 0

Photographed on 03/21/2003. -- Documentation of research installations on the aircraft. L2003-851: Cirrus SR22X - bulkhead penetration in right firewall for engine sensor wires. L2003-852: Cirrus SR22X - fuel flow meter & manifold pressure transducer mounted on upper right side of engine. L2003-853: Cirrus SR22X - optical RPM sensor inside front engine baffle by alternator pulley & belt. L2003-854: Cirrus SR22X - right wing at wingtip attach point. Forward conduit for wires/pitot-static...
Topics: AIRCRAFT DESIGN. -- AIRCRAFT STRUCTURES., What -- Magnetometer, What -- S 15, What -- Dash
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 32

favorite 0

comment 0

Photographed on 03/21/2003. -- Documentation of research installations on the aircraft. L2003-851: Cirrus SR22X - bulkhead penetration in right firewall for engine sensor wires. L2003-852: Cirrus SR22X - fuel flow meter & manifold pressure transducer mounted on upper right side of engine. L2003-853: Cirrus SR22X - optical RPM sensor inside front engine baffle by alternator pulley & belt. L2003-854: Cirrus SR22X - right wing at wingtip attach point. Forward conduit for wires/pitot-static...
Topics: AIRCRAFT DESIGN. -- AIRCRAFT STRUCTURES., What -- Magnetometer, What -- S 15, What -- Dash
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 40

favorite 0

comment 0

Photographed on 03/21/2003. -- Documentation of research installations on the aircraft. L2003-851: Cirrus SR22X - bulkhead penetration in right firewall for engine sensor wires. L2003-852: Cirrus SR22X - fuel flow meter & manifold pressure transducer mounted on upper right side of engine. L2003-853: Cirrus SR22X - optical RPM sensor inside front engine baffle by alternator pulley & belt. L2003-854: Cirrus SR22X - right wing at wingtip attach point. Forward conduit for wires/pitot-static...
Topics: AIRCRAFT DESIGN. -- AIRCRAFT STRUCTURES., What -- Magnetometer, What -- S 15, What -- Dash
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 25

favorite 0

comment 0

Photographed on 03/21/2003. -- Documentation of research installations on the aircraft. L2003-851: Cirrus SR22X - bulkhead penetration in right firewall for engine sensor wires. L2003-852: Cirrus SR22X - fuel flow meter & manifold pressure transducer mounted on upper right side of engine. L2003-853: Cirrus SR22X - optical RPM sensor inside front engine baffle by alternator pulley & belt. L2003-854: Cirrus SR22X - right wing at wingtip attach point. Forward conduit for wires/pitot-static...
Topics: AIRCRAFT DESIGN. -- AIRCRAFT STRUCTURES., What -- Magnetometer, What -- S 15, What -- Dash
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 26

favorite 0

comment 0

Photographed on 03/21/2003. -- Documentation of research installations on the aircraft. L2003-851: Cirrus SR22X - bulkhead penetration in right firewall for engine sensor wires. L2003-852: Cirrus SR22X - fuel flow meter & manifold pressure transducer mounted on upper right side of engine. L2003-853: Cirrus SR22X - optical RPM sensor inside front engine baffle by alternator pulley & belt. L2003-854: Cirrus SR22X - right wing at wingtip attach point. Forward conduit for wires/pitot-static...
Topics: AIRCRAFT DESIGN. -- AIRCRAFT STRUCTURES., What -- Magnetometer, What -- S 15, What -- Dash
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 40

favorite 0

comment 0

Photographed on 03/21/2003. -- Documentation of research installations on the aircraft. L2003-851: Cirrus SR22X - bulkhead penetration in right firewall for engine sensor wires. L2003-852: Cirrus SR22X - fuel flow meter & manifold pressure transducer mounted on upper right side of engine. L2003-853: Cirrus SR22X - optical RPM sensor inside front engine baffle by alternator pulley & belt. L2003-854: Cirrus SR22X - right wing at wingtip attach point. Forward conduit for wires/pitot-static...
Topics: AIRCRAFT DESIGN. -- AIRCRAFT STRUCTURES., What -- Magnetometer, What -- S 15, What -- Dash
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 28

favorite 0

comment 0

Photographed on 03/21/2003. -- Documentation of research installations on the aircraft. L2003-851: Cirrus SR22X - bulkhead penetration in right firewall for engine sensor wires. L2003-852: Cirrus SR22X - fuel flow meter & manifold pressure transducer mounted on upper right side of engine. L2003-853: Cirrus SR22X - optical RPM sensor inside front engine baffle by alternator pulley & belt. L2003-854: Cirrus SR22X - right wing at wingtip attach point. Forward conduit for wires/pitot-static...
Topics: AIRCRAFT DESIGN. -- AIRCRAFT STRUCTURES., What -- Magnetometer, What -- S 15, What -- Dash
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 49

favorite 0

comment 0

Photographed on 03/21/2003. -- Documentation of research installations on the aircraft. L2003-851: Cirrus SR22X - bulkhead penetration in right firewall for engine sensor wires. L2003-852: Cirrus SR22X - fuel flow meter & manifold pressure transducer mounted on upper right side of engine. L2003-853: Cirrus SR22X - optical RPM sensor inside front engine baffle by alternator pulley & belt. L2003-854: Cirrus SR22X - right wing at wingtip attach point. Forward conduit for wires/pitot-static...
Topics: AIRCRAFT DESIGN. -- AIRCRAFT STRUCTURES., What -- Magnetometer, What -- S 15, What -- Dash
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 63

favorite 0

comment 0

Photographed on 03/21/2003. -- Documentation of research installations on the aircraft. L2003-851: Cirrus SR22X - bulkhead penetration in right firewall for engine sensor wires. L2003-852: Cirrus SR22X - fuel flow meter & manifold pressure transducer mounted on upper right side of engine. L2003-853: Cirrus SR22X - optical RPM sensor inside front engine baffle by alternator pulley & belt. L2003-854: Cirrus SR22X - right wing at wingtip attach point. Forward conduit for wires/pitot-static...
Topics: AIRCRAFT DESIGN. -- AIRCRAFT STRUCTURES., What -- Magnetometer, What -- S 15, What -- Dash
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 90

favorite 0

comment 0

Photographed on 03/21/2003. -- Documentation of research installations on the aircraft. L2003-851: Cirrus SR22X - bulkhead penetration in right firewall for engine sensor wires. L2003-852: Cirrus SR22X - fuel flow meter & manifold pressure transducer mounted on upper right side of engine. L2003-853: Cirrus SR22X - optical RPM sensor inside front engine baffle by alternator pulley & belt. L2003-854: Cirrus SR22X - right wing at wingtip attach point. Forward conduit for wires/pitot-static...
Topics: AIRCRAFT DESIGN. -- AIRCRAFT STRUCTURES., What -- Magnetometer, What -- S 15, What -- Dash
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 66

favorite 0

comment 0

Photographed on 03/21/2003. -- Documentation of research installations on the aircraft. L2003-851: Cirrus SR22X - bulkhead penetration in right firewall for engine sensor wires. L2003-852: Cirrus SR22X - fuel flow meter & manifold pressure transducer mounted on upper right side of engine. L2003-853: Cirrus SR22X - optical RPM sensor inside front engine baffle by alternator pulley & belt. L2003-854: Cirrus SR22X - right wing at wingtip attach point. Forward conduit for wires/pitot-static...
Topics: AIRCRAFT DESIGN. -- AIRCRAFT STRUCTURES., What -- Magnetometer, What -- S 15, What -- Dash
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 32

favorite 0

comment 0

Photographed on 03/21/2003. -- Documentation of research installations on the aircraft. L2003-851: Cirrus SR22X - bulkhead penetration in right firewall for engine sensor wires. L2003-852: Cirrus SR22X - fuel flow meter & manifold pressure transducer mounted on upper right side of engine. L2003-853: Cirrus SR22X - optical RPM sensor inside front engine baffle by alternator pulley & belt. L2003-854: Cirrus SR22X - right wing at wingtip attach point. Forward conduit for wires/pitot-static...
Topics: AIRCRAFT DESIGN. -- AIRCRAFT STRUCTURES., What -- Magnetometer, What -- S 15, What -- Dash
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 31

favorite 0

comment 0

Photographed on 03/21/2003. -- Documentation of research installations on the aircraft. L2003-851: Cirrus SR22X - bulkhead penetration in right firewall for engine sensor wires. L2003-852: Cirrus SR22X - fuel flow meter & manifold pressure transducer mounted on upper right side of engine. L2003-853: Cirrus SR22X - optical RPM sensor inside front engine baffle by alternator pulley & belt. L2003-854: Cirrus SR22X - right wing at wingtip attach point. Forward conduit for wires/pitot-static...
Topics: AIRCRAFT DESIGN. -- AIRCRAFT STRUCTURES., What -- Magnetometer, What -- S 15, What -- Dash
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 26

favorite 0

comment 0

Photographed on 03/21/2003. -- Documentation of research installations on the aircraft. L2003-851: Cirrus SR22X - bulkhead penetration in right firewall for engine sensor wires. L2003-852: Cirrus SR22X - fuel flow meter & manifold pressure transducer mounted on upper right side of engine. L2003-853: Cirrus SR22X - optical RPM sensor inside front engine baffle by alternator pulley & belt. L2003-854: Cirrus SR22X - right wing at wingtip attach point. Forward conduit for wires/pitot-static...
Topics: AIRCRAFT DESIGN. -- AIRCRAFT STRUCTURES., What -- Magnetometer, What -- S 15, What -- Dash
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 99

favorite 0

comment 0

Photographed on 03/21/2003. -- Documentation of research installations on the aircraft. L2003-851: Cirrus SR22X - bulkhead penetration in right firewall for engine sensor wires. L2003-852: Cirrus SR22X - fuel flow meter & manifold pressure transducer mounted on upper right side of engine. L2003-853: Cirrus SR22X - optical RPM sensor inside front engine baffle by alternator pulley & belt. L2003-854: Cirrus SR22X - right wing at wingtip attach point. Forward conduit for wires/pitot-static...
Topics: AIRCRAFT DESIGN. -- AIRCRAFT STRUCTURES., What -- Magnetometer, What -- S 15, What -- Dash
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 24

favorite 0

comment 0

Photographed on 03/21/2003. -- Documentation of research installations on the aircraft. L2003-851: Cirrus SR22X - bulkhead penetration in right firewall for engine sensor wires. L2003-852: Cirrus SR22X - fuel flow meter & manifold pressure transducer mounted on upper right side of engine. L2003-853: Cirrus SR22X - optical RPM sensor inside front engine baffle by alternator pulley & belt. L2003-854: Cirrus SR22X - right wing at wingtip attach point. Forward conduit for wires/pitot-static...
Topics: AIRCRAFT DESIGN. -- AIRCRAFT STRUCTURES., What -- Magnetometer, What -- S 15, What -- Dash
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 92

favorite 0

comment 0

Photographed on 03/21/2003. -- Documentation of research installations on the aircraft. L2003-851: Cirrus SR22X - bulkhead penetration in right firewall for engine sensor wires. L2003-852: Cirrus SR22X - fuel flow meter & manifold pressure transducer mounted on upper right side of engine. L2003-853: Cirrus SR22X - optical RPM sensor inside front engine baffle by alternator pulley & belt. L2003-854: Cirrus SR22X - right wing at wingtip attach point. Forward conduit for wires/pitot-static...
Topics: AIRCRAFT DESIGN. -- AIRCRAFT STRUCTURES., What -- Magnetometer, What -- S 15, What -- Dash
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 34

favorite 0

comment 0

Photographed on 03/21/2003. -- Documentation of research installations on the aircraft. L2003-851: Cirrus SR22X - bulkhead penetration in right firewall for engine sensor wires. L2003-852: Cirrus SR22X - fuel flow meter & manifold pressure transducer mounted on upper right side of engine. L2003-853: Cirrus SR22X - optical RPM sensor inside front engine baffle by alternator pulley & belt. L2003-854: Cirrus SR22X - right wing at wingtip attach point. Forward conduit for wires/pitot-static...
Topics: AIRCRAFT DESIGN. -- AIRCRAFT STRUCTURES., What -- Magnetometer, What -- S 15, What -- Dash
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 34

favorite 0

comment 0

Photographed on 03/21/2003. -- Documentation of research installations on the aircraft. L2003-851: Cirrus SR22X - bulkhead penetration in right firewall for engine sensor wires. L2003-852: Cirrus SR22X - fuel flow meter & manifold pressure transducer mounted on upper right side of engine. L2003-853: Cirrus SR22X - optical RPM sensor inside front engine baffle by alternator pulley & belt. L2003-854: Cirrus SR22X - right wing at wingtip attach point. Forward conduit for wires/pitot-static...
Topics: AIRCRAFT DESIGN. -- AIRCRAFT STRUCTURES., What -- Magnetometer, What -- S 15, What -- Dash
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 27

favorite 0

comment 0

Photographed on 03/21/2003. -- Documentation of research installations on the aircraft. L2003-851: Cirrus SR22X - bulkhead penetration in right firewall for engine sensor wires. L2003-852: Cirrus SR22X - fuel flow meter & manifold pressure transducer mounted on upper right side of engine. L2003-853: Cirrus SR22X - optical RPM sensor inside front engine baffle by alternator pulley & belt. L2003-854: Cirrus SR22X - right wing at wingtip attach point. Forward conduit for wires/pitot-static...
Topics: AIRCRAFT DESIGN. -- AIRCRAFT STRUCTURES., What -- Magnetometer, What -- S 15, What -- Dash
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 35

favorite 0

comment 0

Photographed on 03/21/2003. -- Documentation of research installations on the aircraft. L2003-851: Cirrus SR22X - bulkhead penetration in right firewall for engine sensor wires. L2003-852: Cirrus SR22X - fuel flow meter & manifold pressure transducer mounted on upper right side of engine. L2003-853: Cirrus SR22X - optical RPM sensor inside front engine baffle by alternator pulley & belt. L2003-854: Cirrus SR22X - right wing at wingtip attach point. Forward conduit for wires/pitot-static...
Topics: AIRCRAFT DESIGN. -- AIRCRAFT STRUCTURES., What -- Magnetometer, What -- S 15, What -- Dash
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 47

favorite 0

comment 0

Photographed on 03/21/2003. -- Documentation of research installations on the aircraft. L2003-851: Cirrus SR22X - bulkhead penetration in right firewall for engine sensor wires. L2003-852: Cirrus SR22X - fuel flow meter & manifold pressure transducer mounted on upper right side of engine. L2003-853: Cirrus SR22X - optical RPM sensor inside front engine baffle by alternator pulley & belt. L2003-854: Cirrus SR22X - right wing at wingtip attach point. Forward conduit for wires/pitot-static...
Topics: AIRCRAFT DESIGN. -- AIRCRAFT STRUCTURES., What -- Magnetometer, What -- S 15, What -- Dash
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 34

favorite 0

comment 0

Photographed on 03/21/2003. -- Documentation of research installations on the aircraft. L2003-851: Cirrus SR22X - bulkhead penetration in right firewall for engine sensor wires. L2003-852: Cirrus SR22X - fuel flow meter & manifold pressure transducer mounted on upper right side of engine. L2003-853: Cirrus SR22X - optical RPM sensor inside front engine baffle by alternator pulley & belt. L2003-854: Cirrus SR22X - right wing at wingtip attach point. Forward conduit for wires/pitot-static...
Topics: AIRCRAFT DESIGN. -- AIRCRAFT STRUCTURES., What -- Magnetometer, What -- S 15, What -- Dash
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 51

favorite 0

comment 0

Photographed on 03/21/2003. -- Documentation of research installations on the aircraft. L2003-851: Cirrus SR22X - bulkhead penetration in right firewall for engine sensor wires. L2003-852: Cirrus SR22X - fuel flow meter & manifold pressure transducer mounted on upper right side of engine. L2003-853: Cirrus SR22X - optical RPM sensor inside front engine baffle by alternator pulley & belt. L2003-854: Cirrus SR22X - right wing at wingtip attach point. Forward conduit for wires/pitot-static...
Topics: AIRCRAFT DESIGN. -- AIRCRAFT STRUCTURES., What -- Magnetometer, What -- S 15, What -- Dash
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 30

favorite 0

comment 0

Photographed on 03/21/2003. -- Documentation of research installations on the aircraft. L2003-851: Cirrus SR22X - bulkhead penetration in right firewall for engine sensor wires. L2003-852: Cirrus SR22X - fuel flow meter & manifold pressure transducer mounted on upper right side of engine. L2003-853: Cirrus SR22X - optical RPM sensor inside front engine baffle by alternator pulley & belt. L2003-854: Cirrus SR22X - right wing at wingtip attach point. Forward conduit for wires/pitot-static...
Topics: AIRCRAFT DESIGN. -- AIRCRAFT STRUCTURES., What -- Magnetometer, What -- S 15, What -- Dash
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 49

favorite 0

comment 0

Photographed on 03/21/2003. -- Documentation of research installations on the aircraft. L2003-851: Cirrus SR22X - bulkhead penetration in right firewall for engine sensor wires. L2003-852: Cirrus SR22X - fuel flow meter & manifold pressure transducer mounted on upper right side of engine. L2003-853: Cirrus SR22X - optical RPM sensor inside front engine baffle by alternator pulley & belt. L2003-854: Cirrus SR22X - right wing at wingtip attach point. Forward conduit for wires/pitot-static...
Topics: AIRCRAFT DESIGN. -- AIRCRAFT STRUCTURES., What -- Magnetometer, What -- S 15, What -- Dash
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 32

favorite 0

comment 0

Photographed on 03/21/2003. -- Documentation of research installations on the aircraft. L2003-851: Cirrus SR22X - bulkhead penetration in right firewall for engine sensor wires. L2003-852: Cirrus SR22X - fuel flow meter & manifold pressure transducer mounted on upper right side of engine. L2003-853: Cirrus SR22X - optical RPM sensor inside front engine baffle by alternator pulley & belt. L2003-854: Cirrus SR22X - right wing at wingtip attach point. Forward conduit for wires/pitot-static...
Topics: AIRCRAFT DESIGN. -- AIRCRAFT STRUCTURES., What -- Magnetometer, What -- S 15, What -- Dash
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 25

favorite 0

comment 0

NASA Environmental and Energy Conference (part2)
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 23

favorite 0

comment 0

NASA Environmental and Energy Conference (part2)
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 20

favorite 0

comment 0

NASA Environmental and Energy Conference (part2)
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 23

favorite 0

comment 0

NASA Environmental and Energy Conference (part2)
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 24

favorite 0

comment 0

NASA Environmental and Energy Conference (part2)
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 23

favorite 0

comment 0

NASA Environmental and Energy Conference (part2)
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 24

favorite 0

comment 0

NASA Environmental and Energy Conference (part2)
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 24

favorite 0

comment 0

NASA Environmental and Energy Conference (part2)
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 32

favorite 0

comment 0

NASA Environmental and Energy Conference (part2)
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 22

favorite 0

comment 0

NASA Environmental and Energy Conference (part2)
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 22

favorite 0

comment 0

NASA Environmental and Energy conference
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 27

favorite 0

comment 0

NASA Environmental and Energy conference
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 19

favorite 0

comment 0

NASA Environmental and Energy conference
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 34

favorite 0

comment 0

NASA Environmental and Energy conference
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 27

favorite 0

comment 0

NASA Environmental and Energy conference
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 29

favorite 0

comment 0

NASA Environmental and Energy conference
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 24

favorite 0

comment 0

NASA Environmental and Energy conference
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 22

favorite 0

comment 0

NASA Environmental and Energy conference
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 27

favorite 0

comment 0

NASA Environmental and Energy conference
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 24

favorite 0

comment 0

NASA Environmental and Energy conference
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 28

favorite 0

comment 0

NASA Environmental and Energy conference
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 29

favorite 0

comment 0

NASA Environmental and Energy conference
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 18

favorite 0

comment 0

NASA Environmental and Energy conference
Langley Research Center Media Archive
by NASA
image

eye 73

favorite 0

comment 0

Exhibit Specialist Dustin Hitt mans the touchscreen table inside the newly updated NASA Exploration Experience trailer during NASA Exploration Days at Busch Gardens. The trailer offers a 3-D journey through the past, present and into the future of space travel and educates visitors on how technologies developed for space exploration are improving our lives on Earth. Credit: NASA/Sean Smith
Topic: What -- Earth
Source: http://www.nasa.gov/images/content/478788main_iotw-bg-expl-day_full.jpg