Thorsten
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Over the years, I've been reading quite a bit of Shuttle-related material. I've come across the following statement about the transition from RCS yaw jets to rudder in at least 2 hardcover books and 8 different web pages.
At Mach 3.5, the rudder become activated, and the aft RCS yaw jets are deactivated (approximately 45,000 feet).
That's right, the whole world seems to believe it all happens at 45,000 ft.
if you're not familiar with basic aerodynamics, it sounds innocent enough - but 45.000 ft is a bit higher than airliners reach - if you try to fly Mach 3.5 there, not only is drag and heat production enormous, but you'll also screw up your TAEM pattern.
I found it vexing that authors of spaceflight books as well as Shuttle fan pages didn't spot such a glaring typo (the number intended to be given here is probably 145.000 ft) - but they have the best of reference sources for the nonsense:
https://spaceflight.nasa.gov/shuttle/reference/shutref/events/entry/
Yep - NASA describes it that way. And they're not thinking of altering it (I wrote to the webmaster identified in the page index two years ago, my mail just got ignored).
Today I came across another one of the same type, having to do with the SRB sep sequence:
They can also ensure that the Pc - 50 message (chamber pressure greater than 50 psi) correctly appears on the major mode 102 (first stage) ascent trajectory CRT display before SRB separation
https://spaceflight.nasa.gov/shuttle/reference/shutref/events/1stage/
Well, if that were true we'd probably never leave the pad because the SRBs would be disconnected right after ignition. Well, okay, for this one has to know some engineering details to deduce that, but there's another way: I mean, it's not rocket science that a message PC < 50 doesn't mean chamber pressure greater than 50.
Okay - it'd be cheap to mock a few innocent typos - except that they don't get corrected even when someone notifies the page owner, and that they get copy-pasted by space afficinados all around the internet on the grounds that 'NASA wrote it, so it must be true' - that's kinda scary.
At Mach 3.5, the rudder become activated, and the aft RCS yaw jets are deactivated (approximately 45,000 feet).
That's right, the whole world seems to believe it all happens at 45,000 ft.
if you're not familiar with basic aerodynamics, it sounds innocent enough - but 45.000 ft is a bit higher than airliners reach - if you try to fly Mach 3.5 there, not only is drag and heat production enormous, but you'll also screw up your TAEM pattern.
I found it vexing that authors of spaceflight books as well as Shuttle fan pages didn't spot such a glaring typo (the number intended to be given here is probably 145.000 ft) - but they have the best of reference sources for the nonsense:
https://spaceflight.nasa.gov/shuttle/reference/shutref/events/entry/
Yep - NASA describes it that way. And they're not thinking of altering it (I wrote to the webmaster identified in the page index two years ago, my mail just got ignored).
Today I came across another one of the same type, having to do with the SRB sep sequence:
They can also ensure that the Pc - 50 message (chamber pressure greater than 50 psi) correctly appears on the major mode 102 (first stage) ascent trajectory CRT display before SRB separation
https://spaceflight.nasa.gov/shuttle/reference/shutref/events/1stage/
Well, if that were true we'd probably never leave the pad because the SRBs would be disconnected right after ignition. Well, okay, for this one has to know some engineering details to deduce that, but there's another way: I mean, it's not rocket science that a message PC < 50 doesn't mean chamber pressure greater than 50.
Okay - it'd be cheap to mock a few innocent typos - except that they don't get corrected even when someone notifies the page owner, and that they get copy-pasted by space afficinados all around the internet on the grounds that 'NASA wrote it, so it must be true' - that's kinda scary.