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| Started by | Snidely <snidely.too@gmail.com> |
|---|---|
| First post | 2021-11-17 17:58 -0800 |
| Last post | 2021-11-22 15:29 -0800 |
| Articles | 3 — 2 participants |
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40th anniversary of first US manned craft re-use. Snidely <snidely.too@gmail.com> - 2021-11-17 17:58 -0800
Re: 40th anniversary of first US manned craft re-use. JF Mezei <jfmezei.spamnot@vaxination.ca> - 2021-11-17 23:25 -0500
Re: 40th anniversary of first US manned craft re-use. Snidely <snidely.too@gmail.com> - 2021-11-22 15:29 -0800
| From | Snidely <snidely.too@gmail.com> |
|---|---|
| Date | 2021-11-17 17:58 -0800 |
| Subject | 40th anniversary of first US manned craft re-use. |
| Message-ID | <mn.8c367e5b784fcce2.127094@snitoo> |
Well, 5 days ago. STS-2. NasaSpaceFlight.com has a retrospective: <URL:https://www.nasaspaceflight.com/2021/11/sts-2-40th-anniversary/> Turn-around was about 5 months, it seems, but another month was added for tile repairs after RCS hypergolics were spilled. An abort spoiled the Nov 4 date, and the Nov 12 date was also in issue due to mux/demux failure. Launch was 7 months after the STS-1 launch. The flight lasted 2 days instead of the planned 5, due to a fuel cell failure. This was also the first flight where SRB joint o-ring erosion was found. (For JFM, there's a picture of /Columbia/ descending to Edwards. The angle is chosen to give the most appropriate airspeed; I'm not sure what the sink rate for level flight would be if you started trying it at the speed and elevation pictured.) /dps -- "What do you think of my cart, Miss Morland? A neat one, is not it? Well hung: curricle-hung in fact. Come sit by me and we'll test the springs." (Speculative fiction by H.Lacedaemonian.)
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| From | JF Mezei <jfmezei.spamnot@vaxination.ca> |
|---|---|
| Date | 2021-11-17 23:25 -0500 |
| Message-ID | <bBklJ.68377$Wkjc.23879@fx35.iad> |
| In reply to | #9536 |
On 2021-11-17 20:58, Snidely wrote: > (For JFM, there's a picture of /Columbia/ descending to Edwards. The > angle is chosen to give the most appropriate airspeed; Would it be fair to state that the descent rate wouldn't be that different, but by gaining speed, shen they do the final flare up, the wings get the descent rate top drop to near 0 for a smooth landing ? With low airspeed, they wouldn't be able to droop the descent rate by much when they flare up, right ?
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| From | Snidely <snidely.too@gmail.com> |
|---|---|
| Date | 2021-11-22 15:29 -0800 |
| Message-ID | <mn.b3a17e5be0d76f56.127094@snitoo> |
| In reply to | #9537 |
JF Mezei is guilty of <bBklJ.68377$Wkjc.23879@fx35.iad> as of 11/17/2021 8:25:43 PM > On 2021-11-17 20:58, Snidely wrote: > >> (For JFM, there's a picture of /Columbia/ descending to Edwards. The >> angle is chosen to give the most appropriate airspeed; > > > Would it be fair to state that the descent rate wouldn't be that > different, but by gaining speed, shen they do the final flare up, the > wings get the descent rate top drop to near 0 for a smooth landing ? > > With low airspeed, they wouldn't be able to droop the descent rate by > much when they flare up, right ? I'm only an armchair pilot. I would be willing to guess that the CDRs and PLTs have tried this in the simulator, just because, and the crews on the later flights had very much improved simulators. I am willing to guess that trying for level flight is not useful in a Shuttle. /dps -- There's nothing inherently wrong with Big Data. What matters, as it does for Arnold Lund in California or Richard Rothman in Baltimore, are the questions -- old and new, good and bad -- this newest tool lets us ask. (R. Lerhman, CSMonitor.com)
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