visibility Similar

S82E5965 - STS-082 - HST,closeup shots of the telescope during deployment

U.S. Marines with Marine Medium Tiltrotor Squadron

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MODIFIED CENTRIFUGAL IMPELLER AND DIFFUSER EE4528

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TURBINE DEVICE - CONTROL - INSTALLED, NASA Technology Images

Lockheed Martin technicians and engineers in the Vertical Integration Building prepare to hoist the second stage of a Titan IV/Centaur expendable launch vehicle into a vertical position where it can lifted and mated to the first stage of the rocket. The Titan IVB rocket is the newest version of America's most powerful unmanned rocket. This rocket will be used for the Cassini mission to Saturn. The Cassini launch is targeted for October 6 from Launch Complex 40, Cape Canaveral Air Station KSC-97pc661

CONTROL PANEL AND FAN BLADE ON ENGINE IN THE PROPULSION SYSTEMS LABORATORY PSL TANK 1

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NASA Lear Jet Enteisung GRC-2003-C-00127

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Bearbeitetes Kupfer CGR-84 Thruster # GRC-C06-KM (Kinetische Metallisierung) NASA Identifier: C-2007-280

description

Zusammenfassung

Bearbeitetes Kupfer CGR-84 Thruster # GRC-C06-KM (Kinetische Metallisierung)

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Tags

NASA bearbeitetes kupfer cgr 84 strahlruder grc c 06 km kinetische metallisierung divids hohe Auflösung Glenn-Forschungszentrum Luftfahrtforschungsorganisation ultrahohe Auflösung
date_range

Datum

11/09/2009
place

Lage

create

Quelle

Defense Visual Information Distribution Service
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Link

https://www.dvidshub.net/
copyright

Copyright-info

Public Domain Dedication. Public Use Notice of Limitations: https://www.dvidshub.net/about/copyright

label_outline Explore Machined Copper Cgr 84 Thruster Grc C 06 Km Kinetic Metallization, Aviation Research Organization, Glenn Research Center

B-47 NACELLE im ALTITUDE WIND TUNNEL AWT SHOP NASA Identifier: C-1956-42935

ROCKETDYNE ADVANCED REUSUABLE TRANSPORTATION TECHNOLOGY ARTT HYPERSONIC INLET

HIGH ENERGY ROCKET PROPELLANT RUN OF SEVERAL THOUSAND POUNDS THRUST NASA Identifier: C-1955-37428

JET EXIT MODELL IN NIEDRIGER BALANCE KAMMER DES 8X6 FOOT WIND TUNNEL SHOWING PROBE AKTUATOR MECHANISMUS AND JET DEFLECTOR AND EXIT NOZZLES AND SHROUDS NASA Identifier: C-1954-36301

TRANSITION VON IGNITION TO FLAME GROWTH UNTER DREI AUSSENRADIATION IN DREI DIMENSIONEN TIGER-3D TEST ERGEBNISSE VON DEM JAPAN MIKROGRAVITY CENTER JAMIC NASA Identifier: C-1999-803

Übersicht-Einlass mit Einlassführungsschiebergehäuse NASA Identifier: C-2004-688

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LASER (HOLOGRAPHISCHES) SYSTEM IN FORSCHUNGSFORSCHUNG ERB NASA Identifier: C-1984-7191

NASA / PRATT AND WHITNEY LOW NOISE FAN TEST

Themen

NASA bearbeitetes kupfer cgr 84 strahlruder grc c 06 km kinetische metallisierung divids hohe Auflösung Glenn-Forschungszentrum Luftfahrtforschungsorganisation ultrahohe Auflösung