On Wed, May 02, 2007 at 05:54:22AM -0400, DataPacRat wrote:
>The current design I'm fiddling with is 83% fuel. I suppose if the
>fission-fragment has the best Isp, the only options I have left are to
>increase the fuel-to-payload ratio, and/or use some staging to get rid
>of some of the unnecessary structural mass in mid-thrust.

That seems like a very low fuel fraction; designs I've heard about are
99% or more.

>(My mistake in typing that out - that's supposed to be fully-loaded
>sAccel times burn-time.)

Of course, you should also bear in mind that the mass of the drive will
be a factor - you may want to stick with Orions in the end, because that
f-f thruster itself weighs 140lb/lbthr as opposed to 0.125lb/lbthr for
the Orion. Certainly worth considering both.

>On 02/05/07, Roger Burton West <[EMAIL PROTECTED]> wrote:
>>Um, no. The whole point is that you lose mass as you go along.
>I'm quite aware, but the 'Simplified Delta-V' is a bit quicker for an
>order-of-magnitude comparison between different drives.

But goes increasingly wrong as the fuel fraction increases...

>I'm not quite up to fiddling with GVB's formulas in that manner yet. :)

It's really easy. Trust me on this.

(1) Make sure your drive and fuel tank are in the same subassembly (or
package).

(2) Right-click the package and select "new link node".

(3) Select in the four list windows: the drive, "vFUEL_WEIGHT", the
fuel, "TotalPayload". Leave the multiplier at 1.

That's all it takes, and you'll get an accurate delta_V readout.

R
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