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Design and Stress Analysis of Extraterrestrial ... - The Black Vault

Design and Stress Analysis of Extraterrestrial ... - The Black Vault

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<strong>Extraterrestrial</strong> motors in power from I to 50 kW are promising<br />

with thermoemission, thermoelectric energy conversion with any<br />

nonnuclear heat source. Radioisotope power sources are effective<br />

for systems with thermoelectric energy converters for low-power<br />

motors (from 30 W to 50 kW).<br />

<strong>The</strong> economy <strong>of</strong> extraterrestrial motors<br />

<strong>The</strong> second important requirement for an ERE is, minimum.<br />

expenditure <strong>of</strong> working medium during its operation, i.e., the best<br />

economy.factor. This is determined by the specific function <strong>of</strong><br />

the worki'ng medium.<br />

Specific consumption is<br />

the ratio <strong>of</strong> the flow rate per second<br />

<strong>of</strong> the working medium to the thrust level <strong>of</strong> the motor (kg/N-s):<br />

C,,Mr. (1.2)<br />

In an electrical ERE the entire reserve <strong>of</strong> the working medium<br />

is located aboard the ship, therefore, we determine the economy<br />

factor <strong>of</strong> a motor based on the specific impulse.<br />

<strong>The</strong> specific impulse <strong>of</strong> a motor is the ratio <strong>of</strong> its thrust to<br />

the flow rate per second <strong>of</strong> the working medium: J = R/m T This<br />

value is inverse to the specific flow rate <strong>of</strong> the working medium.<br />

Specific impulse in<br />

the International System is<br />

WIz=[A N-s/kg (1.3)<br />

Table 1.2 givesa comparison <strong>of</strong> the specific impulses <strong>of</strong> plasma<br />

extraterrestrial engines (PEE), ion extraterrestrial engines (IEE),<br />

<strong>and</strong> liquid propellant rocket engines (LPRE).<br />

Ak-7

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