These pictures needless to say they brought back memories. Up until I was promoted into management most of the time didn't seem like work.
I was on the TRE-2 crew when we tested the Redstone engine that put John Glen ( Friendship 7 ) in orbit.
I was assigned as the Leadman on TRE-1 second shift at the start of the H-1 R&D and ended up on the day shift Leadman. The instability problem was one of many. The H-1 engine powered the Saturn vehicle in a cluster of 8 engines, which had to start all at the same time. They started with two squibs on a solid propellant gas generator and bootstrapped to provide hot gas driving the turban for main propellant pumps during main stage. It was some time while working TRE-1, that I started thinking it was up to me to get us to the moon. It was good times with the promotion to supervision in the TRE Area. I knew the engines and all the men that made up the crews, and we were working three shifts. Things were to good to last. I was transferred to the Bowl Area, Liquid Hydrogen, J-2 engine, Major Test Stand Conversions, Contractors. This was work, and we didn't have an area Super, we reported to our hard nosed Group Leader, actually he was a good guy. The Bowl area J-2 program was the first time ever that liquid hydrogen had been used in such a huge amount, thousands gallons at a time. Part of the J-2 program included a demonstration simulated altitude shut down and restart on VTS-3A. Other J-2 R&D testing on VTS-3B. VTS-2 ran J-2 production testing. Large engine tests support for the X-15 were ran on HTS.
Things started to slow down after J-2. I was assigned to CTL-3 second shift running Aero Spike engine tests
Next was Bravo Area second shift running stability testing on the RS-18 Lunar assent engine.
Then Third shift for SSFL and out the gate in 1969. And on to Caterpillar. At least this is how I think I remember the period.
Smokeless flame juts from the diffuser of a unique vacuum chamber in which the upper stage rocket engine, the hydrogen fueled J-2, was tested at a simulated space altitude in excess of 60,000 feet. The smoke you see is actually steam. In operation, vacuum is established by injecting steam into the chamber and is maintained by the thrust of the engine firing through the diffuser. The engine was tested in this environment for start, stop, coast, restart, and full-duration operations. The chamber was located at Rocketdyne's Propulsion Field Laboratory, in the Santa Susana Mountains, near Canoga Park, California. The J-2 engine was developed by Rocketdyne for the Marshall Space Flight Center.
Up until I was promoted into management most of the time didn't seem like work.
I was on the TRE-2 crew when we tested the Redstone engine that put John Glen ( Friendship 7 ) in orbit.
I was assigned as the Leadman on TRE-1 second shift at the start of the H-1 R&D and ended up on the day shift Leadman.
The instability problem was one of many. The H-1 engine powered the Saturn vehicle in a cluster of 8 engines, which had to start all at the same time. They started with two squibs on a solid propellant gas generator and bootstrapped to provide hot gas driving the turban for main propellant pumps during main stage. It was some time while working TRE-1, that I started thinking it was up to me to get us to the moon.
It was good times with the promotion to supervision in the TRE Area. I knew the engines and all the men that made up the crews, and we were working three shifts.
Things were to good to last. I was transferred to the Bowl Area, Liquid Hydrogen, J-2 engine, Major Test Stand Conversions, Contractors.
This was work, and we didn't have an area Super, we reported to our hard nosed Group Leader, actually he was a good guy.
The Bowl area J-2 program was the first time ever that liquid hydrogen had been used in such a huge amount, thousands gallons at a time.
Part of the J-2 program included a demonstration simulated altitude shut down and restart on VTS-3A. Other J-2 R&D testing on VTS-3B.
VTS-2 ran J-2 production testing. Large engine tests support for the X-15 were ran on HTS.
Things started to slow down after J-2. I was assigned to CTL-3 second shift running Aero Spike engine tests
Next was Bravo Area second shift running stability testing on the RS-18 Lunar assent engine.
Then Third shift for SSFL and out the gate in 1969. And on to Caterpillar.
At least this is how I think I remember the period.