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VARIABLE VALVE TIMING - ULTRASONIC FUEL VAPORIZATION - IGNITION SYSTEMS

VARIABLE VALVE TIMING - ULTRASONIC FUEL VAPORIZATION - IGNITION SYSTEMS

VARIABLE VALVE TIMING - ULTRASONIC FUEL VAPORIZATION - IGNITION SYSTEMS

VARIABLE VALVE TIMING - ULTRASONIC FUEL VAPORIZATION - IGNITION SYSTEMS

TILT NACELLE VTOL - VERTICAL TAKE OFF LANDING - A AIRCRAFT PROPULSION SYSTEM

TURBINE BED FUEL SYSTEM IN THE HIGH PRESSURE FACILITY HPF

DISPLAY OF PROTECTIVE SYSTEM UNIT AT FIRE STATION

DISPLAY OF PROTECTIVE SYSTEM UNIT AT FIRE STATION

TURBINE BED FUEL SYSTEM IN THE HIGH PRESSURE FACILITY HPF

VARIABLE VALVE TIMING - ULTRASONIC FUEL VAPORIZATION - IGNITION SYSTEMS

description

Summary

The original finding aid described this as:

Capture Date: 9/30/1976

Keywords: Larsen Scan

Photographs Relating to Agency Activities, Facilities and Personnel

label_outline

Tags

variable valve timing variable valve timing ultrasonic fuel vaporization ultrasonic fuel vaporization ignition systems nasa national aeronautics and space administration high resolution ultra high resolution ignition systems nasa photographs space program 1970 s us national archives
date_range

Date

1976
create

Source

The U.S. National Archives
link

Link

https://catalog.archives.gov/
copyright

Copyright info

No known copyright restrictions

label_outline Explore Vaporization, Ultrasonic, Timing

A ground crew crouches atop a palllet of mail on Forward

A detailed view of the weapons load of an F-16C Falcon from the 52nd Fighter Wing based at Spandahlem AB Germany as it takes on fuel from a 100th Air Expeditionary Wing KC-135R Stratotanker (not shown) from RAF Mildenhall United Kingdom on 31 Mar 99. While patroling the skies over Kosovo during Operation Allied Force, it is armed with AIM-120C missiles on the two outboard stations for self protection and Highspeed Anti Radiation Missiles on the inboard station to suppress anti-aircraft radar sites

An aerial view of the Air Force Rocket Propulsion Laboratory, Air Force Systems Command, as a rocket is launched during a test

STS075-393-031 - STS-075 - Radiative Ignition and Transition to Spread Investigation (RITSI)

STS091-333-007 - STS-091 - The new superlightweight external fuel tank after separation from Discovery

STS091-333-005 - STS-091 - The new superlightweight external fuel tank after separation from Discovery

Interior view of the laser device compartment aboard the NKC-135 airborne laser laboratory (ALL) aircraft in flight. In the foreground is the laser device and the laser fuel tanks are in the background

STS055-256-021 - STS-055 - External Fuel Tank Separation

COLD PIPE IN THE PROPULSION SYSTEMS LABORATORY PSL TANK 3 - TRAVERSING PROBE - PULSE JETS

SOLAR HEAT DRAWINGS, NASA Technology Images

EMPLOYEES IN THE MATERIAL AND PROCESS CONTROL BRANCH FOR STORY IN LEWIS NEWS NEWSLETTER

FUEL INJECTOR, NASA Technology Images

Topics

variable valve timing variable valve timing ultrasonic fuel vaporization ultrasonic fuel vaporization ignition systems nasa national aeronautics and space administration high resolution ultra high resolution ignition systems nasa photographs space program 1970 s us national archives