visibility Similar

STS053-242-004 - STS-053 - MDDK FARE experiment

STS053-245-024 - STS-053 - FARE MDDK experiment

STS073-334-030 - STS-073 - Tunnel between crew compartment and Spacelab

Ares 1-X segment US2 being transported from building 50 to building 333

STS053-249-017 - STS-053 - FARE experiment. in the MDDK

STS057-59-003 - STS-057 - Detail views of the Fluid Acquisition and Supply Equipment (FARE) experiment.

STS057-59-037 - STS-057 - Detail views of the Fluid Acquisition and Supply Equipment (FARE) experiment.

Fries Manaufacturing & Power Company, Idols Station, Yadkin River, Clemmons, Forsyth County, NC

STS084-319-014 - STS-084 - Orbiter Docking System (ODS) interior and hatches

code Related

30 CM CENTIMETER GIMBAL VIBRATION TEST IN THE DYNAMICS LABORATORY IN THE 8X6 FOOT WIND TUNNEL BUILDING

30 CM CENTIMETER GIMBAL VIBRATION TEST IN THE DYNAMICS LABORATORY IN THE 8X6 FOOT WIND TUNNEL BUILDING

30 CM CENTIMETER GIMBAL VIBRATION TEST IN THE DYNAMICS LABORATORY IN THE 8X6 FOOT WIND TUNNEL BUILDING

VIBRATOR UNITS IN STRUCTURAL DYNAMICS LABORATORY IN THE 8X6 FOOT WIND TUNNEL BUILDING

8 INCH BOATTAIL NOZZLE IN THE 8X6 FOOT WIND TUNNEL TEST SECTION

VTOL VERTICAL TAKE OFF LANDING TEST FACILITIES AT THE 8X6 FOOT WIND TUNNEL

TEST SETUP IN THE 8X6 FOOT WIND TUNNEL BALANCE CHAMBER AND TEST SECTION FOR THE BOUNDARY LAYER CONTROL INLET

TEST SETUP IN THE 8X6 FOOT WIND TUNNEL BALANCE CHAMBER AND TEST SECTION FOR THE BOUNDARY LAYER CONTROL INLET

TEST SETUP IN THE 8X6 FOOT WIND TUNNEL BALANCE CHAMBER AND TEST SECTION FOR THE BOUNDARY LAYER CONTROL INLET

30 CM CENTIMETER GIMBAL VIBRATION TEST IN THE DYNAMICS LABORATORY IN THE 8X6 FOOT WIND TUNNEL BUILDING

description

Summary

The original finding aid described this as:

Capture Date: 4/14/1978

Photographer: MARTIN BROWN

Keywords: Larsen Scan

Location Building No: 54

Photographs Relating to Agency Activities, Facilities and Personnel

Nothing Found.

label_outline

Tags

centimeter gimbal vibration test cm centimeter gimbal vibration test dynamics laboratory dynamics laboratory foot building nasa rocket technology rocket development wind tunnel national aeronautics and space administration high resolution ultra high resolution photographer foot wind tunnel building martin brown nasa photographs space program 1970 s us national archives
date_range

Date

1978
create

Source

The U.S. National Archives
link

Link

https://catalog.archives.gov/
copyright

Copyright info

No known copyright restrictions

label_outline Explore Foot Wind Tunnel Building, Gimbal, Dynamics

SECTIONS OF A DISECTED 20 FOOT WOOD WIND TURBINE BLADE SECTION

8 CM CENTIMETER ION ENGINE - VACUUM FACILITY TANK 5 IN THE ELECTRIC PROPULSION LABORATORY EPL

CONFIGURATION AND INSTALLATION OF 5.5 INCH SONIC INLET IN THE 9X15 FOOT WIND TUNNEL

30 CM CENTIMETER PPU POWER PROCESSING UNIT LOAD SIMULATOR AND SEQUENCE MULTIPLEXER ELECTRONICS BOX

Facility operators Earl Sine and Joe Manson and CPT Ray Pope (left to right) operate the master control console for 50-megawatt wind tunnel testing. The technicians work in the Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Flight Control Division, Air Force Systems Command

8X6 FOOT WIND TUNNEL FOR LEWIS NEWS NEWSLETTER STORY ABOUT THE 30TH ANNIVERSARY

CONSTRUCTION AT THE AEROSPACE INFORMATION AND DISPLAY AID BUILDING - ROCKET COMBUSTION LABORATORY RCL - ROCKET ENGINE TEST FACILITY RETF - 8X6 FOOT WIND TUNNEL MODEL PREPARATION BUILDING - CRYOGENIC EQUIPMENT & VEHICLE REPAIR BUILDING

ROTOR DYNAMICS FACILITY, NASA Technology Images

VENT 5-2 WITH BOUNDARY LAYER TRIP MODEL IN THE 8X6 FOOT WIND TUNNEL

MOD-0 ON 100 FOOT TOWER SHOWING NEW BLADES AND TOWER FIXTURE

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, United Space Alliance worker Dan Kenna (right) positions a Reinforced Carbon Carbon panel on the table to perform flash thermography. In the background, Paul Ogletree observes the monitor. Attached to the leading edge of the wing of the orbiters, the gray carbon composite RCC panels have sufficient strength to withstand the aerodynamic forces experienced during launch and reentry, which can reach as high as 800 pounds per square foot. The operating range of RCC is from minus 250º F to about 3,000º F, the temperature produced by friction with the atmosphere during reentry.

ACOUSTIC PANEL ROTATING MICROPHONIC INSTALLATION IN THE 9X15 FOOT WIND TUNNEL

Topics

centimeter gimbal vibration test cm centimeter gimbal vibration test dynamics laboratory dynamics laboratory foot building nasa rocket technology rocket development wind tunnel national aeronautics and space administration high resolution ultra high resolution photographer foot wind tunnel building martin brown nasa photographs space program 1970 s us national archives