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The Complete Book of Spaceflight: From Apollo 1 to Zero Gravity

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300 nuclear propulsion<br />

propulsion) or indirectly (see nuclear-electric propulsion).<br />

Research on nuclear power systems for prospective<br />

space applications began in the 1950s. Early American<br />

research on RTGs and space nuclear reac<strong>to</strong>rs was conducted<br />

under the auspices <strong>of</strong> the SNAP program. More<br />

recently, the SP-100 program focused on the design <strong>of</strong><br />

larger reac<strong>to</strong>rs for use in space. With one exception, the<br />

United States has flown nuclear material aboard spacecraft<br />

only <strong>to</strong> power RTGs and RHUs: SNAPSHOT was<br />

the only American space mission ever <strong>to</strong> carry a working<br />

nuclear reac<strong>to</strong>r. By contrast, numerous Soviet RORSAT<br />

missions have been reac<strong>to</strong>r-powered. 86<br />

nuclear propulsion<br />

<strong>The</strong> use <strong>of</strong> energy released by a nuclear reaction <strong>to</strong> provide<br />

thrust directly, as distinct from nuclear-electric propulsion.<br />

A nuclear propulsion system derives its thrust from<br />

the products <strong>of</strong> nuclear fission or fusion, 169 and was first<br />

seriously studied by Stanislaw Ulam and Frederick de<br />

H<strong>of</strong>fman in 1944 as a spin<strong>of</strong>f <strong>of</strong> their work on the Manhattan<br />

Project. During the quarter century following<br />

World War II, the A<strong>to</strong>mic Energy Commission (superseded<br />

by the Department <strong>of</strong> Energy in 1974) worked with<br />

various federal agencies on a series <strong>of</strong> nuclear engine projects,<br />

culminating in NERVA.<br />

One way <strong>to</strong> achieve nuclear propulsion is <strong>to</strong> heat a<br />

working fluid by pumping it through a nuclear reac<strong>to</strong>r<br />

and then let the fluid expand through a nozzle. Considering<br />

that nuclear fission fuel contains more than a million<br />

times as much energy per unit mass as chemical fuel<br />

does, this sounds promising. But the approach is limited<br />

by the temperature at which a reac<strong>to</strong>r and key components<br />

<strong>of</strong> a rocket, such as a nozzle, can operate. <strong>The</strong> best<br />

working fluid <strong>to</strong> use is hydrogen, because it is the lightest<br />

substance and therefore, at any given temperature, consists<br />

<strong>of</strong> the fastest-moving particles. Chemical rockets<br />

cannot produce hydrogen as an exhaust, because hydrogen<br />

is not the sole product <strong>of</strong> any practical chemical reaction.<br />

With unlimited nuclear power, however, it is not<br />

necessary <strong>to</strong> react or burn anything; instead, hydrogen<br />

gas could simply be heated inside a nuclear reac<strong>to</strong>r and<br />

then ejected as a high-speed exhaust. This was the idea <strong>of</strong><br />

the NERVA project. 1<br />

Other concepts in nuclear propulsion have sought <strong>to</strong><br />

circumvent the temperature limitation inherent in circulating<br />

the working fluid around a reac<strong>to</strong>r by harnessing<br />

the power <strong>of</strong> runaway nuclear reactions. <strong>The</strong> most important<br />

and promising <strong>of</strong> these is the nuclear pulse rocket.<br />

nuclear pulse rocket<br />

A rocket propelled by a rapid and lengthy series <strong>of</strong> small<br />

a<strong>to</strong>mic or nuclear explosions. A variety <strong>of</strong> schemes have<br />

been proposed since the 1940s. Project Orion was the<br />

longest study—involving actual model test flights—<strong>of</strong> the<br />

nuclear pulse concept based on fission. Project Daedalus<br />

provided a counterpart based on fusion.<br />

Nuclear Rocket Development Station (NRDS)<br />

A NASA-AEC (A<strong>to</strong>mic Energy Commission) facility<br />

concerned with performing research and development<br />

work on nuclear-powered rocket engines, such as the<br />

KIWI series, <strong>to</strong> be used from upper-stage space flight<br />

propulsion. <strong>The</strong> test site is located at Jackass Flats, which<br />

is approximately 95 km northeast <strong>of</strong> Las Vegas, Nevada.<br />

nuclear-electric propulsion (NEP)<br />

A form <strong>of</strong> electric propulsion in which the electrical<br />

energy used <strong>to</strong> accelerate the propellant comes from a<br />

nuclear power source, such as a space-based nuclear<br />

reac<strong>to</strong>r.<br />

nucleus<br />

<strong>The</strong> center <strong>of</strong> an a<strong>to</strong>m, around which orbits a cloud <strong>of</strong><br />

electrons. It consists <strong>of</strong> pro<strong>to</strong>ns and neutrons bound<br />

<strong>to</strong>gether by the strong force. Under the right conditions,<br />

nuclei may undergo nuclear fission or fusion, with the<br />

release <strong>of</strong> large amounts <strong>of</strong> energy.<br />

NUSAT (Northern Utah Satellite)<br />

An air traffic control radar calibration satellite built by<br />

Weber State University (WSU) and Utah State University<br />

(USU) students and staff at Ogden, Utah. It was deployed<br />

from a modified Get-Away Special canister on the Space<br />

Shuttle Challenger.NUSAT measured 48 cm in diameter<br />

and was an 18-sided cylinder. It orbited for 20 months<br />

until reentering on December 15, 1986, and it demonstrated<br />

that satellites could be built small, simple, and at<br />

low cost for special applications. With this satellite, WSU<br />

and USU shared the claim <strong>to</strong> be the first American university<br />

<strong>to</strong> place a satellite in space.<br />

Shuttle deployment<br />

Date: April 29, 1985<br />

Mission: STS-51B<br />

Orbit: 318 × 339 km × 57.0°<br />

Mass: 54 kg

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