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SLS Test: Stennis team overview path to RS-25 engine ignition
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Topic: SLS Test: Stennis team overview path to RS-25 engine ignition (Read 2667 times)
Chris Bergin
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SLS Test: Stennis team overview path to RS-25 engine ignition
«
on:
08/13/2015 01:00 am »
http://www.nasaspaceflight.com/2015/08/sls-test-stennis-team-overview-rs25-ignition/
Lots of quotes and info here, thanks to Philip Sloss, who is at Stennis for test six of seven (covered in the RS-25 update thread)....but this is worthy of a standalone article.
---
Articles on this path:
http://www.nasaspaceflight.com/tag/ssme/
RS-25 Test Update Thread:
http://forum.nasaspaceflight.com/index.php?topic=35220.0
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Rocket Science
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Re: SLS Test: Stennis team overview path to RS-25 engine ignition
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Reply #1 on:
08/13/2015 01:20 am »
Excellent primer article for the test Philip, lots of meaty details!
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Chris Bergin
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"The laws of physics are unforgiving"
~Rob: Physics instructor, Aviator
robertross
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Re: SLS Test: Stennis team overview path to RS-25 engine ignition
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Reply #2 on:
08/13/2015 02:03 am »
Huh, something I didn't know (and previously thought about):
“We run (the engine test) off of facility liquid oxygen run tanks and fuel (liquid hydrogen) tanks, but we also have interconnected piping that allows us to back-feed those systems during a hot-fire from barge tanks."
Nice article Philip!
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rcoppola
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Re: SLS Test: Stennis team overview path to RS-25 engine ignition
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Reply #3 on:
08/13/2015 02:15 am »
Great article. This engine will be so well tested and understood within the context of it's new role, that I really look forward to what they'll be able to do with the next expendable version.
Regardless, 4 instead of 3, directly under the tanks as opposed to the shuttle off-set and all sitting between 7 Million pounds of SRB hell on earth. This is going to be one hell of a show.
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