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INTERIOR OF THE AEROSPACE INFORMATION & DISPLAY AID BUILDING

PROCESS PIPING IN THE PROPULSION SYSTEMS LABORATORY EQUIPMENT BUILDING PSLEB AND THE ICING RESEARCH TUNNEL IRT

10X10 FOOT WIND TUNNEL COMPUTER COMPLEX

VERTICAL LIFT FACILITY

10X10 FOOT WIND TUNNEL COMPUTER COMPLEX

PIPING UNDER PHOTOGRAPHIC LABORATORY

PROCESS PIPING IN THE PROPULSION SYSTEMS LABORATORY EQUIPMENT BUILDING PSLEB AND THE ICING RESEARCH TUNNEL IRT

CONSTRUCTION

SPACE SHUTTLE MODEL IN THE 10X10 FOOT WIND TUNNEL

QUIET ENGINE

DAMAGE TO NO. 1 COOLER AT THE 10X10 FOOT WIND TUNNEL

INTERIOR OF THE AEROSPACE INFORMATION & DISPLAY AID BUILDING

CONSTRUCTION

PROCESS PIPING IN THE PROPULSION SYSTEMS LABORATORY EQUIPMENT BUILDING PSLEB AND THE ICING RESEARCH TUNNEL IRT

FAN BLADES AND FAN BLADE HUB

PIPING UNDER PHOTOGRAPHIC LABORATORY

PROCESS PIPING IN THE PROPULSION SYSTEMS LABORATORY EQUIPMENT BUILDING PSLEB AND THE ICING RESEARCH TUNNEL IRT

10X10 FOOT WIND TUNNEL COMPUTER COMPLEX

CHAMBER AND WORK PROGRAM - ZERO GRAVITY FACILITY

EXPERIMENTAL TEST RIGS IN THE PROPULSION SYSTEMS LABORATORY PSL SHOP AND ACCESS BUILDING TANKS 1 AND 2

PIPING UNDER PHOTOGRAPHIC LABORATORY

PROCESS PIPING IN THE PROPULSION SYSTEMS LABORATORY EQUIPMENT BUILDING PSLEB AND THE ICING RESEARCH TUNNEL IRT

CHAMBER AND WORK PROGRAM - ZERO GRAVITY FACILITY

EXPERIMENTAL TEST RIGS IN THE PROPULSION SYSTEMS LABORATORY PSL SHOP AND ACCESS BUILDING TANKS 1 AND 2

PANELED AREA OF F-106 AIRPLANE IN THE HANGAR

J-58 EMISSIONS COLLECTION TUBE

PANELED AREA OF F-106 AIRPLANE IN THE HANGAR

CHAMBER AND WORK PROGRAM - ZERO GRAVITY FACILITY

PROCESS PIPING IN THE PROPULSION SYSTEMS LABORATORY EQUIPMENT BUILDING PSLEB AND THE ICING RESEARCH TUNNEL IRT

PROCESS PIPING IN THE PROPULSION SYSTEMS LABORATORY EQUIPMENT BUILDING PSLEB AND THE ICING RESEARCH TUNNEL IRT

EXPERIMENTAL TEST RIGS IN THE PROPULSION SYSTEMS LABORATORY PSL SHOP AND ACCESS BUILDING TANKS 1 AND 2

10X10 FOOT WIND TUNNEL COMPUTER COMPLEX

PROCESS PIPING IN THE PROPULSION SYSTEMS LABORATORY EQUIPMENT BUILDING PSLEB AND THE ICING RESEARCH TUNNEL IRT

CHAMBER AND WORK PROGRAM - ZERO GRAVITY FACILITY

PANELED AREA OF F-106 AIRPLANE IN THE HANGAR

QUIET ENGINE

PROCESS PIPING IN THE PROPULSION SYSTEMS LABORATORY EQUIPMENT BUILDING PSLEB AND THE ICING RESEARCH TUNNEL IRT

DAMAGE TO NO. 1 COOLER AT THE 10X10 FOOT WIND TUNNEL

FAN BLADES AND FAN BLADE HUB

PROCESS PIPING IN THE PROPULSION SYSTEMS LABORATORY EQUIPMENT BUILDING PSLEB AND THE ICING RESEARCH TUNNEL IRT

PIPING UNDER PHOTOGRAPHIC LABORATORY

PROCESS PIPING IN THE PROPULSION SYSTEMS LABORATORY EQUIPMENT BUILDING PSLEB AND THE ICING RESEARCH TUNNEL IRT

DAMAGE TO NO. 1 COOLER AT THE 10X10 FOOT WIND TUNNEL

CHAMBER AND WORK PROGRAM - ZERO GRAVITY FACILITY

CONSTRUCTION

EXPERIMENTAL TEST RIGS IN THE PROPULSION SYSTEMS LABORATORY PSL SHOP AND ACCESS BUILDING TANKS 1 AND 2

RESEARCH FACILITY - CELL 21 OF THE OLD ROCKET LABORATORY ORL

PROCESS PIPING IN THE PROPULSION SYSTEMS LABORATORY EQUIPMENT BUILDING PSLEB AND THE ICING RESEARCH TUNNEL IRT

PANELED AREA OF F-106 AIRPLANE IN THE HANGAR

EXPERIMENTAL TEST RIGS IN THE PROPULSION SYSTEMS LABORATORY PSL SHOP AND ACCESS BUILDING TANKS 1 AND 2

PANELED AREA OF F-106 AIRPLANE IN THE HANGAR

RESEARCH FACILITY - CELL 21 OF THE OLD ROCKET LABORATORY ORL

PANELED AREA OF F-106 AIRPLANE IN THE HANGAR

SPACE SHUTTLE MODEL IN THE 10X10 FOOT WIND TUNNEL

CHAMBER AND WORK PROGRAM - ZERO GRAVITY FACILITY

FAN BLADES AND FAN BLADE HUB

CONSTRUCTION

FAN BLADES AND FAN BLADE HUB

PROCESS PIPING IN THE PROPULSION SYSTEMS LABORATORY EQUIPMENT BUILDING PSLEB AND THE ICING RESEARCH TUNNEL IRT

PANELED AREA OF F-106 AIRPLANE IN THE HANGAR

RESEARCH FACILITY - CELL 21 OF THE OLD ROCKET LABORATORY ORL

INTERIOR OF THE AEROSPACE INFORMATION & DISPLAY AID BUILDING

VARIOUS EQUIPMENT IN THE ENGINE RESEARCH BUILDING ERB - HIGH ENERGY FUEL LABORATORY HEFL - AEROSPACE INFORMATION AND DISPLAY AID BUILDING

STORAGE BUILDING ANNEX - RECEIVING AND SHIPPING BUILDING CONSTRUCTION - ROCKET COMBUSTION LABORATORY RCL

PRE-CONSTRUCTION IN TEST CELL SE-17 AND CONTROL ROOM IN THE ENGINE RESEARCH BUILDING ERB

SETUPS LOCATED IN THE FRACTURE MECHANICS LABORATORY AND THE HIGH LOAD TENSILE TESTING FACILITY IN THE SOUTH 40 AREA

TURBINE IN VACUUM CHAMBER

PAPER DRYING PROJECT - B-2 FACILITY NATIONAL RECORD CENTER FIRE - NASA PLUM BROOK STATION SANDUSKY OHIO

STORAGE BUILDING ANNEX - RECEIVING AND SHIPPING BUILDING CONSTRUCTION - ROCKET COMBUSTION LABORATORY RCL

RIG AND COMPONENTS

SERVICE AWARDS CEREMONY

COMMUNICATION TECHNOLOGY SATELLITE CTS PROJECT - TANK 5 OF THE ELECTRIC PROPULSION LABORATORY EPL

QUIET ENGINE BACK JET INSTALLATION

CONSTRUCTION AT THE ENGINE RESEARCH BUILDING ERB SOUTHWEST SW WING AND OUTSIDE FOUNDATIONS

MAGNETO HYDRODYNAMICS MHD RIG IN OPERATION - ROCKET FIRING

BBN CAVITY NOISE TEST AT THE 8X6 FOOT WIND TUNNEL

QUIET ENGINE BACK JET INSTALLATION

FATIGUE TEST SECTION

SOUTH SIDE OF THE 8X6 FOOT WIND TUNNEL TEST SECTION

PLASMA IN RIG

RF AMPLIFIER TUBE - COMMUNICATION TECHNOLOGY SATELLITE CTS OST SERIAL NO. 0 - ON ACCEPTANCE TEST BENCH

1 FAN BLADE FROM NO. 4 CT

18 FOOT DIAMETER WORK PLATFORM IN THE 8X6 FOOT WIND TUNNEL FACILITY

CONSTRUCTION AT THE PHOTOGRAPHIC BRANCH

9X15 FOOT WIND TUNNEL VERTICAL SHORT TAKE OFF LANDING VSTOL SONIC INLET TEST INSTALLATION

DETERIORATED CONDITIONS IN ZERO GRAVITY FACILITY

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

SPACE POWER FACILITY SPF VACUUM TECHNOLOGY LABORATORY

SEAL DRYING RIG

AERSPACE INFORMATION AND DISPLAY AID BUILDING WEST SIDE SCAFFOLDING

MULTI LAYER BLANKET INSTALLATION IN FUEL PIT AT THE ROCKET ENGINE TEST FACILITY RETF

BRICK WORK AT THE AEROSPACE INFORMATION AND DISPLAY AID BUILDING FOR REHAB STUDY

CONFERENCE ROOM IN SOUTHWEST WING OF THE DEVELOPMENT ENGINEERING BUILDING DEB

LIQUID OXYGEN FLOW TEST RIG AT HYDRAULICS LABORATORY IN THE F SITE TEST BUILDING

ZERO GRAVITY FACILITY CHAMBER

NEW CONSTRUCTION IN THE ENGINE RESEARCH BUILDING ERB SOUTHWEST SW EXTENSION

BACK PRESSURE DEVICE IN THE FABRICATION SHOP

MODEL NOZZLE CONFIGURATION OF GENERAL ELECTRIC GE FLUIDYNE SUPPRESSOR NOZZLE AT THE 8X6 FOOT WIND TUNNEL

THRUST REVERSER AIRPLANE MODEL IN THE 9X15 FOOT WIND TUNNEL

BRAYTON ROTATING UNIT BRU ENGINE - BRAYTON CYCLE