Re: MMU Question

From: Jorge R. Frank (jrfrank_at_ibm-pc.borg)
Date: 03/29/05


Date: Tue, 29 Mar 2005 08:02:43 -0600


"Joe D." <joe@nospam.invalid> wrote in
news:wi61e.90558$%Y4.19280@bignews6.bellsouth.net:

> "Keith F. Lynch" <kfl@KeithLynch.net> wrote in message
> news:d22mkc$rlj$1@panix1.panix.com...
>>
>> What if the MMU gets stuck in the on position? Does the shuttle have
>> enough delta-V to catch him after the MMU gas is all expended? Could
>> it cause reentry? How much spin could a malfunctioning MMU put on an
>> astronaut, and what could be done if that happens? Thanks.
>
> MMU had about 80 ft/sec total delta V, so even if 100% was expended
> in a linear runaway the orbiter should have enough OMS delta V to
> retrieve. In general OMS delta V is about 20x that, but it varies
> based on propellant load and whether any is expended on ascent.

The OMS delta-V capability is actually around 1000 fps, or about 12x that
of the MMU.

-- 
JRF
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check "Organization" (I am not assimilated) and
think one step ahead of IBM.


Relevant Pages

  • Re: MMU Question
    ... > enough delta-V to catch him after the MMU gas is all expended? ... in a linear runaway the orbiter should have enough OMS delta V to ... In general OMS delta V is about 20x that, ... In theory it could build up very high pitch/yaw/roll rates, ...
    (sci.space.shuttle)
  • Re: MMU Question
    ... >> itself, mind you, because the MMU is highly redundant). ... sets of thrusters, precisely to permit dealing with such situations), and ... uses the other side to stop the spin. ... probably the orbiter comes and gets him, to minimize demands on the MMU ...
    (sci.space.shuttle)

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