SATURN SIVB STAGE INDEX


SIVB COMPONENTS
Sheet One
 

Wire Harness Assembly and Electronic System Testing



Plug connector is primed for resin backing.

Connector is placed in holding tool.

Resin is applied into plug connector to secure wires.

Technicians assembling wire harness for SIVB 506.

Technicians assembling wire harness for SIVB 506.

Production acceptance testing area.

Propellant utilization system being tested.

Test of Fuel Tank Pressurization Control Module at Atomics International, Canoga Park, CA.

Specimen under test.

|Close up of test specimen.
(Images files are approximately 300K to 500K in size)

Auxiliary Propulsion System, SIVB Retro-Rocket Motors
& Aft Skirt Hydrogen Burner Testing



Technicians working on APS modules in the A45 Maintenance and Assembly building (July, 1967).

Storage, modification and check-out of SIVB APS modules in the Maintenance and Assembly building.

APS module approaching the Gamma Site for reinstallation and firing.

APS module is removed from Gamma Test Cell III.

Smaller crane lifts APS module onto handling fixture.

APS module is placed in protective container at Alpha I, site III.

APS unit installed on shaker unit at Alpha I, site III.

APS on shaker unit at Alpha I, site III.

APS on shaker unit in tangential axis at Alpha I, site III.

APS on shaker unit at Alpha I, site III.

Technician in protective suit examines APS unit during leak check after vibration test at Alpha I, site III.

APS installed in "thrust axis" on the M-B vibration unit.

APS during "burp firing" at Gamma Test Cell III.

APS during horizontal "burp firing" at Gamma Test Cell III.

Thiokol control center, Elkton Maryland.

Retro-rocket motor is installed in Thiokol test cell (1967).

Effects of combustion on motor liner.

Retro-rocket motor nozzle.

SIVB 505 LH2/O2 burner is installed on edge of thrust structure.

SIVB 505 LH2/O2 burner installed.
 

Sheet Two

 

SATURN SIVB STAGE INDEX