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Responsive Access Small Cargo Affordable Launch (RASCAL ...

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payload at the 270 nmi circular orbit. An advantage to this alternative is that the upper<br />

stages will become smaller each performing a smaller ∆V. A disadvantage of this<br />

approach is that the fourth stage will add dry mass to the system as well as involve<br />

another component that could fail. This could result in a lower total system reliability.<br />

This alternative could result in an increased cost due to the addition of the extra stage.<br />

(The GT <strong>RASCAL</strong> cost analysis will show this cost is actually made up for in the weight<br />

reduction). This alternative configuration was closed in the internal iteration loop of the<br />

DSM and this alternative resulted in the overall payload capacity of the baseline<br />

<strong>RASCAL</strong> design increasing from 52 lbs to 211 lbs.<br />

Alternative 4:<br />

The fourth alternative involves combining the LOX hybrid with the fourth stage<br />

kick motor. This will carry the advantages of improving the upper stages without altering<br />

the first stage design. It will result in a slightly more expensive rocket than the baseline,<br />

but will start to approach the payload numbers set out in the <strong>RASCAL</strong> program. This<br />

alternative configuration was closed in the internal iteration loop of the DSM and this<br />

alternative resulted in the overall payload capacity of the baseline <strong>RASCAL</strong> design<br />

increasing from 52 lbs to 224 lbs.<br />

Alternative 5:<br />

The fifth and final alternative involves combining the LOX hybrid with the fourth<br />

stage kick motor and the MMC upper stage. This design should result in the highest<br />

performance since it uses all of the enhancing alternatives presented. This alternative<br />

should also result in the most expensive vehicle since the LOX hybrid adds length to the<br />

first stage, the fourth stage adds the cost of a new stage, and the new MMC technology<br />

needs to be matured. When this configuration was closed in the internal iteration loop the<br />

DSM the payload increased from 52 lbs to 303 lbs. This is above the desired 250 lbs of<br />

payload set out in the <strong>RASCAL</strong> goal. This higher payload means that this alternative can<br />

be further scaled down to achieve the 250 lb goal.<br />

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