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Shuttle leading edge protection
Was there any thought given to a Boost Protective Cover type solution? I'd think the leading edges might be covered until after the tank and SRB's are gone, then ejected. -- A host is a host from coast to & no one will talk to a host that's close........[v].(301) 56-LINUX Unless the host (that isn't close).........................pob 1433 is busy, hung or dead....................................20915-1433 |
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David Lesher wrote: Was there any thought given to a Boost Protective Cover type solution? I'd think the leading edges might be covered until after the tank and SRB's are gone, then ejected. If you are going to keep the jettisonable wing gloves on until the ET is jettisoned, that's virtually all the way to orbit, and they would be a weight penalty; if you jettison them while still under power from the SSMEs then the gloves themselves become a collision hazard with the orbiter, like the foam did....but it is an interesting thought.... Pat |
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Pat Flannery wrote in
: David Lesher wrote: Was there any thought given to a Boost Protective Cover type solution? I'd think the leading edges might be covered until after the tank and SRB's are gone, then ejected. If you are going to keep the jettisonable wing gloves on until the ET is jettisoned, that's virtually all the way to orbit, and they would be a weight penalty; if you jettison them while still under power from the SSMEs then the gloves themselves become a collision hazard with the orbiter, like the foam did....but it is an interesting thought.... Right. You have to ensure the cover jettisons when it's supposed to, and doesn't jettison when it isn't supposed to. Cogratulations David Lesher, you've just created two new Crit-1 failure modes for a vehicle that already has plenty! Now, there *are* alternatives that do make sense, such as using an aerodynamic fairing attached to the ET to cover the RCC during ascent. Such a fairing could be designed to separate cleanly from the orbiter along with the rest of the ET during ET sep. It could also "pay for its own mass" by reducing parasitic drag on the stack during ascent. -- JRF Reply-to address spam-proofed - to reply by E-mail, check "Organization" (I am not assimilated) and think one step ahead of IBM. |
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Pat Flannery wrote:
David Lesher wrote: Was there any thought given to a Boost Protective Cover type solution? I'd think the leading edges might be covered until after the tank and SRB's are gone, then ejected. If you are going to keep the jettisonable wing gloves on until the ET is jettisoned, that's virtually all the way to orbit, and they would be a weight penalty; if you jettison them while still under power from the SSMEs then the gloves themselves become a collision hazard with the orbiter, like the foam did....but it is an interesting thought.... The bipod ramp foam came off and interacted with the turbulent airflow between the ET and the orbiter. At some point doesn't the airflow become negligent, i.e. past the densest part of the atmosphere? Wouldn't anything coming off the ET after that point go straight back and not encounter any turbulence as the stack accelerates? -- bp Proud Member of the Human O-Ring Society Since 2003 (remove 'dot' in addy for email) |
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