Re: Griffin Wants Inline SDLV and 5 Segment SRB/CEV
- From: Reed Snellenberger <rsnellenberger@xxxxxxxxxxxxxxxxxxxxx>
- Date: Sun, 03 Jul 2005 17:54:29 GMT
"Jorge R. Frank" <jrfrank@xxxxxxxxxxx> wrote in
news:Xns9687830AAF60Fjrfrank@xxxxxxxxxxxxxx:
> Scott Lowther <scottlowther@xxxxxxxxxxxxxxxxxxxxxx> wrote in
> news:M7Axe.343$j21.231@xxxxxxxxxxxxx:
>
>> Kim Keller wrote:
>>
>>>>It wouldn't entirely surprise me to see the first qualification
>>>>launche of the 5-segment stick booster (no upper stage) by late
>>>>2006, using Pad 39B and the third MLP as infrastructure.
>>>
>>>There's no way the avionics and the TVC system will be ready for test
>>>by then.
>>>
>> Errrrrmmmm... the TVC system is available *now.*
>
> In two axes (pitch and yaw, or more precisely rock and tilt) only. A
> single SRB has no roll control.
>
>
I forgot about the earlier discussion on this topic (might have been in
s.s.shuttle) -- roll control would definitely add to the development
time, but would roll control be absolutely necessary to the initial test
flights to qualify the booster itself?
As a follow-up question -- is "active" roll control needed (i.e., "we're
going to roll the booster 120 degrees after liftoff"), or simply enough
control for "roll prevention"? How much does returning to an
axisymmetric payload simplify the guidance problem -- in particular, we
no longer have to worry about things like wing loading, etc?
--
I was punching a text message into my | Reed Snellenberger
phone yesterday and thought, "they need | GPG KeyID: 5A978843
to make a phone that you can just talk | rsnellenberger
into." Major Thomb | -at-houston.rr.com
.
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