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Systems for Nuclear Auxiliary Power
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<h2 id="odd-numbered-snaps-radioisotope-thermoelectric-generators">Odd-numbered SNAPs: radioisotope thermoelectric generators</h2> <p><a href="/facts/Radioisotope_thermoelectric_generators/Tsjjvp5h">Radioisotope thermoelectric generators</a> use the heat of <a href="/facts/Radioactive_decay/Ya6FVjt4">radioactive decay</a> to produce electricity. </p> <h3>SNAP-1</h3> <p>SNAP-1 was a test platform that was never deployed, using <a href="/facts/Cerium-144/n2LF751R">cerium-144</a> in a <a href="/facts/Rankine_cycle/HBWjXS0n">Rankine cycle</a> with <a href="/facts/Mercury_(element)/WlxfoHva">mercury</a> as the <a href="/facts/Coolant/531hqfUQ">heat transfer fluid</a>. Operated successfully for 2500 hours.<a class="footnote-ref" id="fnref:5" href="#fn:5"><sup>5</sup></a> </p> <h3>SNAP-3</h3> <p>SNAP-3 was the first <a href="/facts/Radioisotope_thermoelectric_generator/Tsjjvp5h">RTG</a> used in a space mission (1961). Launched aboard <a href="/facts/U.S._Navy/xYK0fUou">U.S. Navy</a> <a href="/facts/Transit_(satellite)/tXAvVaWb">Transit 4A and 4B navigation satellites</a>. The electrical output of this RTG was 2.5 watts.<a class="footnote-ref" id="fnref:6" href="#fn:6"><sup>6</sup></a> </p> <h3>SNAP-7</h3> <p>SNAP-7A, D and F was designed for marine applications such as lighthouses and buoys;<a class="footnote-ref" id="fnref:7" href="#fn:7"><sup>7</sup></a> at least six units were deployed in the mid-1960s, with names SNAP-7A through SNAP-7F. SNAP-7D produced thirty watts of electricity<a class="footnote-ref" id="fnref:8" href="#fn:8"><sup>8</sup></a> using 225 <a href="/facts/Curie_(unit)/LeS60aVv">kilocuries</a> (8.3 <a href="/facts/Becquerel/4C3yrsqp">PBq</a>)<a class="footnote-ref" id="fnref:9" href="#fn:9"><sup>9</sup></a> (about four kilograms) of <a href="/facts/Strontium-90/VJNoC5eR">strontium-90</a> as SrTiO3. These were very large units, weighing between 1,870 and 6,000 pounds (850 and 2,720 kg).<a class="footnote-ref" id="fnref:10" href="#fn:10"><sup>10</sup></a> </p> <h3>SNAP-9</h3> <p>After SNAP-3 on Transit 4A/B, SNAP-9A units served aboard many of the <a href="/facts/Transit_(satellite)/tXAvVaWb">Transit satellite</a> series. In April 1964 a SNAP-9A failed to achieve orbit and disintegrated, dispersing roughly 1 kilogram (2.2 lb) of <a href="/facts/Plutonium-238/JzY7TPFE">plutonium-238</a> over all continents. Most plutonium fell in the southern hemisphere. Estimated 630 <a href="/facts/TBq/4C3yrsqp">TBq</a> or 2100 person-Sv of radiation was released.<a class="footnote-ref" id="fnref:11" href="#fn:11"><sup>11</sup></a><a class="footnote-ref" id="fnref:12" href="#fn:12"><sup>12</sup></a><a class="footnote-ref" id="fnref:13" href="#fn:13"><sup>13</sup></a><a class="footnote-ref" id="fnref:14" href="#fn:14"><sup>14</sup></a> </p> <h3>SNAP-11</h3> <p>SNAP-11 was an experimental <a href="/facts/Radioisotope_thermoelectric_generator/Tsjjvp5h">RTG</a> intended to power the <a href="/facts/Surveyor_program/98RNqFN3">Surveyor</a> probes during the lunar night. The <a href="/facts/Curium-242/WnMh6VLE">curium-242</a> RTGs would have produced 25 watts of electricity using 900 watts of thermal energy for 130 days. The hot junction temperature was 925 °F (496 °C; 769 K), the cold junction temperature was 350 °F (177 °C; 450 K). They had a liquid <a href="/facts/NaK/09HKRf44">NaK</a> thermal control system and a movable shutter to dump excess heat.<a class="footnote-ref" id="fnref:15" href="#fn:15"><sup>15</sup></a><a class="footnote-ref" id="fnref:16" href="#fn:16"><sup>16</sup></a> They were not used on the Surveyor missions.<a class="footnote-ref" id="fnref:17" href="#fn:17"><sup>17</sup></a> </p> <blockquote><p>In general, the SNAP 11 fuel block is a cylindrical multi-material unit which occupies the internal volume of the generator. TZM (molybdenum alloy) fuel capsule, fueled with <a href="/facts/Curium-242/WnMh6VLE">curium-242</a> (Cm2O3 in an iridium matrix) is located in the center of the fuel block. Capsule is surrounded by a platinum sphere, approximately 2+1⁄4 inches in diameter, which provides shielding and acts as an energy absorber for impact considerations. This assembly is enclosed in graphite and beryllium sub-assemblies to provide the proper thermal distribution and ablative protection.<a class="footnote-ref" id="fnref:18" href="#fn:18"><sup>18</sup></a></p></blockquote> <h3>SNAP-19</h3> <p>SNAP-19(B) was developed for the <a href="/facts/Nimbus_program/wPM5TACR">Nimbus-B satellite</a> by the Nuclear Division of the Martin-Marietta Company<a class="footnote-ref" id="fnref:19" href="#fn:19"><sup>19</sup></a> (now Teledyne Energy Systems). Fueled with plutonium-238, two parallel lead telluride thermocouple generators produced an initial maximum of approximately 30 watts of electricity.<a class="footnote-ref" id="fnref:20" href="#fn:20"><sup>20</sup></a> Nimbus 3 used a SNAP-19B with the recovered fuel from the Nimbus-B1 attempt.<a class="footnote-ref" id="fnref:21" href="#fn:21"><sup>21</sup></a> </p><p>SNAP-19's powered the <i><a href="/facts/Pioneer_10/om14fT0h">Pioneer 10</a></i> and <i><a href="/facts/Pioneer_11/9QgrnSWp">Pioneer 11</a></i> missions.<a class="footnote-ref" id="fnref:22" href="#fn:22"><sup>22</sup></a> They used n-type 2N-PbTe and p-type TAGS-85 thermoelectric elements.<a class="footnote-ref" id="fnref:23" href="#fn:23"><sup>23</sup></a> </p><p>Modified SNAP-19B's were used for the <i><a href="/facts/Viking_1/lBbblTgw">Viking 1</a></i> and <i><a href="/facts/Viking_2/3L9AGV2z">Viking 2</a></i> landers.<a class="footnote-ref" id="fnref:24" href="#fn:24"><sup>24</sup></a> </p><p>A SNAP-19C was used to power a telemetry array at <a href="/facts/Nanda_Devi/5DxCt7nN">Nanda Devi</a> in <a href="/facts/Uttarakhand/n3juS1z4">Uttarakhand</a> for a CIA operation to track Chinese missile launches.<a class="footnote-ref" id="fnref:25" href="#fn:25"><sup>25</sup></a> </p> <h3>SNAP-21 & 23</h3> <p>SNAP-21<a class="footnote-ref" id="fnref:26" href="#fn:26"><sup>26</sup></a> and SNAP-23 were designed for underwater use<a class="footnote-ref" id="fnref:27" href="#fn:27"><sup>27</sup></a><a class="footnote-ref" id="fnref:28" href="#fn:28"><sup>28</sup></a> and used <a href="/facts/Strontium-90/VJNoC5eR">strontium-90</a> as the radioactive source, encapsulated as either <a href="/facts/Strontium_oxide/hxr7KKj5">strontium oxide</a> or <a href="/facts/Strontium_titanate/fQ4lC197">strontium titanate</a>. They produced about ten watts of electricity. </p> <h3>SNAP-27</h3> <p>Five SNAP-27 units provided electric power for the <a href="/facts/Apollo_Lunar_Surface_Experiments_Package/TDJprc7B">Apollo Lunar Surface Experiments Packages</a> (ALSEP) left on the Moon by <a href="/facts/Apollo_program/IC1Ek1Ao">Apollo</a> <a href="/facts/Apollo_12/TyLvYjhw">12</a>, <a href="/facts/Apollo_14/SuokTzAu">14</a>, <a href="/facts/Apollo_15/8h2QMY4z">15</a>, <a href="/facts/Apollo_16/XQY3CDnf">16</a>, and <a href="/facts/Apollo_17/5szGEz7n">17</a>. The SNAP-27 power supply weighed about 20 kilograms, was 46 cm long and 40.6 cm in diameter. It consisted of a central fuel capsule surrounded by concentric rings of thermocouples. Outside of the thermocouples was a set of fins to provide for heat rejection from the cold side of the thermocouple. Each of the SNAP devices produced approximately 75 W of electrical power at 30 VDC. The energy source for each device was a rod of plutonium-238 providing a thermal power of approximately 1250 W.<a class="footnote-ref" id="fnref:29" href="#fn:29"><sup>29</sup></a> This fuel capsule, containing 3.8 kilograms (8.4 lb) of <a href="/facts/Plutonium-238/JzY7TPFE">plutonium-238</a> in oxide form (44,500 <a href="/facts/Curie_(unit)/LeS60aVv">Ci</a> or 1.65 <a href="/facts/Petabecquerel/4C3yrsqp">PBq</a>), was carried to the Moon in a separate fuel cask attached to the side of the <a href="/facts/Lunar_Module/XtvQS5K5">Lunar Module</a>. The fuel cask provided thermal insulation and added structural support to the fuel capsule. On the Moon, the Lunar Module pilot removed the fuel capsule from the cask and inserted it in the RTG. </p><p>These stations transmitted information about <a href="/facts/Moonquake/NAtC34tW">moonquakes</a> and meteor impacts, lunar magnetic and gravitational fields, the Moon's internal temperature, and the Moon's atmosphere for several years after the missions. After ten years, a SNAP-27 still produced more than 90% of its initial output of 75 watts. </p><p>The fuel cask from the SNAP-27 unit carried by the <a href="/facts/Apollo_13/YfSNWC07">Apollo 13</a> mission currently lies in 20,000 feet (6,100 m) of water at the bottom of the <a href="/facts/Tonga_Trench/8aQ9TsmX">Tonga Trench</a> in the <a href="/facts/Pacific_Ocean/bdxgXRVM">Pacific Ocean</a>. This mission failed to land on the Moon, and the <a href="/facts/Lunar_module/XtvQS5K5">lunar module</a> carrying its generator burnt up during re-entry into the Earth's atmosphere, with the trajectory arranged so that the cask would land in the trench. The cask survived re-entry, as it was designed to do,<a class="footnote-ref" id="fnref:30" href="#fn:30"><sup>30</sup></a> and no release of plutonium has been detected. The corrosion resistant materials of the capsule are expected to contain it for 10 half-lives (870 years).<a class="footnote-ref" id="fnref:31" href="#fn:31"><sup>31</sup></a> </p> <h2 id="even-numbered-snaps-compact-nuclear-reactors">Even-numbered SNAPs: compact nuclear reactors</h2> <p>A series of compact nuclear reactors intended for space use, the even numbered SNAPs were developed for the U.S. government by the <a href="/facts/Atomics_International/EQTYTE3a">Atomics International</a> division of <a href="/facts/North_American_Aviation/zY6IG0pa">North American Aviation</a>. </p> <h3>SNAP Experimental Reactor (SER)</h3> <p>The SNAP Experimental Reactor (SER) was the first reactor to be built by the specifications established for space satellite applications. The SER used <a href="/facts/Uranium_zirconium_hydride/onXT8f3s">uranium zirconium hydride</a> as the fuel and <a href="/facts/Eutectic/UFbecnqo">eutectic</a> sodium-potassium alloy (<a href="/facts/NaK/09HKRf44">NaK</a>) as the coolant and operated at approximately 50 kW thermal. The system did not have a power conversion but used a secondary heat air blast system to dissipate the heat to the atmosphere. The SER used a similar reactor reflector moderator device as the <a href="/facts/SNAP-10A/GBUqQYUU">SNAP-10A</a> but with only one reflector. Criticality was achieved in September 1959 with final shutdown completed in December 1961. The project was considered a success. It gave continued confidence in the development of the SNAP Program and it also led to in depth research and component development. </p> <h3>SNAP-2</h3> <p>The SNAP-2 Developmental Reactor was the second SNAP reactor built. This device used Uranium-zirconium hydride fuel and had a design reactor power of 55 kWt. It was the first model to use a flight control assembly and was tested from April 1961 to December 1962. The basic concept was that nuclear power would be a long term source of energy for crewed space capsules. However, the crew capsule had to be shielded from deadly radiation streaming from the nuclear reactor. Surrounding the reactor with a radiation shield was out of the question. It would be far too heavy to launch with the rockets available at that time. To protect the "crew" and "payload", the SNAP-2 system used a "shadow shield". The shield was a truncated cone containing <a href="/facts/Lithium_hydride/uWCl2pST">lithium hydride</a>. The reactor was at the small end and the crew capsule/payload was in the shadow of the large end.<a class="footnote-ref" id="fnref:32" href="#fn:32"><sup>32</sup></a> </p><p>Studies were performed on the reactor, individual components and the support system. Atomics International, a division of North American Aviation did the development and testing work. The SNAP-2 Shield Development unit was responsible for developing the radiation shield. Creating the shield meant melting lithium hydride and casting it into the form required. The form was a big truncated cone. Molten lithium hydride had to be poured into the casting mold a little at a time otherwise it would crack as it cooled and solidified. Cracks in the shield material would be fatal to any space crew or payload depending on it because it would allow radiation to stream through to the crew/payload compartment. As the material cooled, it would form kind of a hollowed vortex in the middle. The development engineers had to create ways to fill the vortex while maintaining the shield's integrity. And, in doing all this they had to keep in mind that they were working with a material that could be explosively unstable in a moist oxygen rich environment. Analysis also revealed that under thermal and radiation gradients, the lithium hydride could disassociate and hydrogen ions could migrate through the shield. This would produce variations of shielding efficacy and could subject the payloads to intense radiation. Efforts were made to mitigate these effects. </p><p>The SNAP 2DR used a similar reactor reflector moderator device as the <a href="/facts/SNAP-10A/GBUqQYUU">SNAP-10A</a> but with two movable and internal fixed reflectors. The system was designed so that the reactor could be integrated with a mercury Rankine cycle to generate 3.5 kW of electricity. </p> <h3>SNAP-8</h3> <p>The SNAP-8 reactors were designed, constructed and operated by Atomics International under contract with the <a href="/facts/National_Aeronautics_and_Space_Administration/TIMCV0yV">National Aeronautics and Space Administration</a>. Two SNAP-8 reactors were produced: The SNAP 8 Experimental Reactor and the SNAP 8 Developmental Reactor. Both SNAP 8 reactors used the same highly enriched uranium zirconium hydride fuel as the SNAP 2 and SNAP 10A reactors. The SNAP 8 design included primary and secondary NaK loops to transfer heat to the <a href="/facts/Mercury_(element)/WlxfoHva">mercury</a> <a href="/facts/Rankine_cycle/HBWjXS0n">rankine</a> power conversion system. The electrical generating system for the SNAP 8 reactors was supplied by <a href="/facts/Aerojet_General/hlrJsgVF">Aerojet General</a>.<a class="footnote-ref" id="fnref:33" href="#fn:33"><sup>33</sup></a> </p><p>The SNAP 8 Experimental Reactor was a 600 kWt reactor that was tested from 1963 to 1965. </p><p>The SNAP 8 Developmental Reactor had a reactor core measuring 9.5 by 33 inches (24 by 84 cm), contained a total of 18 pounds (8.2 kg) of fuel, had a power rating of 1 MWt. The reactor was tested in 1969 at the <a href="/facts/Santa_Susana_Field_Laboratory/2cAjQWWV">Santa Susana Field Laboratory</a>.<a class="footnote-ref" id="fnref:34" href="#fn:34"><sup>34</sup></a> </p> <h3>SNAP-10A</h3> <p class="note">Main article: <a href="/facts/SNAP-10A/GBUqQYUU">SNAP-10A</a></p> <p>The SNAP-10A was a space-qualified nuclear reactor power system launched into space in 1965 under the SNAPSHOT program.<a class="footnote-ref" id="fnref:35" href="#fn:35"><sup>35</sup></a><a class="footnote-ref" id="fnref:36" href="#fn:36"><sup>36</sup></a> It was built as a research project for the Air Force, to demonstrate the capability to generate higher power than RTGs. The reactor employed two moveable beryllium reflectors for control, and generated 35 kWt at beginning of life. The system generated electricity by circulating NaK around lead tellurium thermocouples. To mitigate launch hazards, the reactor was not started until it reached a safe orbit. </p><p>SNAP-10A was launched into Earth orbit in April 1965, and used to power an <a href="/facts/RM-81_Agena/mRvYKtC1">Agena-D</a> research satellite, built by Lockheed/Martin. The system produced 500W of electrical power during an abbreviated 43-day flight test. The reactor was prematurely shut down by a faulty command receiver. It is predicted to remain in orbit for 4,000 years.<a class="footnote-ref" id="fnref:37" href="#fn:37"><sup>37</sup></a> </p> <h2 id="see-also">See also</h2> <ul><li><a href="/facts/List_of_nuclear_power_systems_in_space/vVKRntoR">List of nuclear power systems in space</a></li> <li><a href="/facts/Nuclear_power_in_space/fgMCeMsu">Nuclear power in space</a></li></ul> <h2 id="citations">Citations</h2> <h2 id="general-sources">General sources</h2> <ul><li><a href="https://web.archive.org/web/20100609000421/http://nuclear.mst.edu/department/spacepower.html">"Nuclear Power in Space". U.S. Department of Energy, Office of Nuclear Energy, Science & Technology</a></li></ul> <h2 id="external-links">External links</h2> Wikimedia Commons has media related to Systems for Nuclear Auxiliary Power. <ul><li><a href="https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19720007958_1972007958.pdf">SNAP-8 Electrical Generating System Development Program, Final Report</a></li> <li><a href="https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19740072136_1974072136.pdf">SNAP-19, Phase 3. Quarterly Progress Report, 1 January – 31 March 1966</a></li> <li><a href="http://hdl.handle.net/2060/19740072135">SNAP 19, Phase 3. Quarterly Progress Report, 1 Apr. – 30 Jun. 1966</a></li> <li><a href="http://hdl.handle.net/2060/19760073679">Analysis of the need for Agena command destruct and/or generator eject systems on the Nimbus B/SNAP-19 mission</a></li> <li><a href="http://hdl.handle.net/2060/19680022615">SNAP-19/Nimbus B integration experience</a></li> <li><a href="http://hdl.handle.net/2060/19730065642">SNAP-27, Volume 1. Quarterly Report, 1 Jul. – 30 Sep. 1966</a></li> <li><a href="http://hdl.handle.net/2060/19730065466">SNAP-27, Volume 2. Quarterly Report, 1 Jan. – 31 Mar. 1966</a></li> <li><a href="http://www.fas.org/nuke/space/bennett0706.pdf">"Space Nuclear Power: Opening the Final Frontier"</a> by G. L. Bennett (2006)</li> <li><a href="https://web.archive.org/web/20080619143130/http://www.totse.com/en/technology/space_astronomy_nasa/spacnuke.html">"Space Nuclear Power Sources" (tables)</a></li></ul> <h2 id="references">References</h2> <ol> <li id="fn:1"><p>J. E. Lipp; Robert M. Salter (March 1954). "Project Feedback Summary Report Volume I". RAND. Retrieved 11 April 2020. <a href="https://www.rand.org/pubs/reports/R262z1.html" target="_blank">https://www.rand.org/pubs/reports/R262z1.html</a> <a href="#fnref:1" class="footnote-back-ref">↩</a></p></li> <li id="fn:2"><p>William R. Corliss (1966). SNAP NUCLEAR POWER REACTORS. U.S. Atomic Energy Commission/Division of Technical Information. <a href="#fnref:2" class="footnote-back-ref">↩</a></p></li> <li id="fn:3"><p>William R. Corliss (1966). SNAP NUCLEAR POWER REACTORS. U.S. Atomic Energy Commission/Division of Technical Information. <a href="#fnref:3" class="footnote-back-ref">↩</a></p></li> <li id="fn:4"><p>"SNAP Overview". U.S. Department of Energy. Retrieved 9 April 2020. <a href="https://www.etec.energy.gov/Operations/Major_Operations/SNAP_Overview.php" target="_blank">https://www.etec.energy.gov/Operations/Major_Operations/SNAP_Overview.php</a> <a href="#fnref:4" class="footnote-back-ref">↩</a></p></li> <li id="fn:5"><p>Schwartz, H. J.; Shure, L. I. (1 January 1965). "Survey of electric power plants for space applications". NTRS - NASA Technical Reports Server. Retrieved 25 April 2024. <a href="https://ntrs.nasa.gov/citations/19660005486" target="_blank">https://ntrs.nasa.gov/citations/19660005486</a> <a href="#fnref:5" class="footnote-back-ref">↩</a></p></li> <li id="fn:6"><p>Schwartz, H. J.; Shure, L. I. (1 January 1965). "Survey of electric power plants for space applications". NTRS - NASA Technical Reports Server. Retrieved 25 April 2024. <a href="https://ntrs.nasa.gov/citations/19660005486" target="_blank">https://ntrs.nasa.gov/citations/19660005486</a> <a href="#fnref:6" class="footnote-back-ref">↩</a></p></li> <li id="fn:7"><p>"Anthropogenic Radioactivity: Major Plume Source Points – RADNET: Section 11". www.davistownmuseum.org. Retrieved 31 March 2018. <a href="http://www.davistownmuseum.org/cbm/Rad8f.html" target="_blank">http://www.davistownmuseum.org/cbm/Rad8f.html</a> <a href="#fnref:7" class="footnote-back-ref">↩</a></p></li> <li id="fn:8"><p>Young, C. N. (15 March 1963). Snap 7d – Strontium-90 Fueled Thermoelectric Generator Power Source. Thirty Watt U.S. Navy Floating Weather Station. Final Report (Report). doi:10.2172/4713816. OSTI 4713816. <a href="https://digital.library.unt.edu/ark:/67531/metadc1029853/" target="_blank">https://digital.library.unt.edu/ark:/67531/metadc1029853/</a> <a href="#fnref:8" class="footnote-back-ref">↩</a></p></li> <li id="fn:9"><p>"Anthropogenic Radioactivity: Major Plume Source Points – RADNET: Section 11". www.davistownmuseum.org. Retrieved 31 March 2018. <a href="http://www.davistownmuseum.org/cbm/Rad8f.html" target="_blank">http://www.davistownmuseum.org/cbm/Rad8f.html</a> <a href="#fnref:9" class="footnote-back-ref">↩</a></p></li> <li id="fn:10"><p>Schwartz, H. J.; Shure, L. I. (1 January 1965). "Survey of electric power plants for space applications". NTRS - NASA Technical Reports Server. Retrieved 25 April 2024. <a href="https://ntrs.nasa.gov/citations/19660005486" target="_blank">https://ntrs.nasa.gov/citations/19660005486</a> <a href="#fnref:10" class="footnote-back-ref">↩</a></p></li> <li id="fn:11"><p>Lovas, Rezső G. (2003). Handbook of nuclear chemistry: Instrumentation, separation techniques environmental iusses. Springer Science & Business Media. p. 308. ISBN 978-1-4020-1317-1. <a href="978-1-4020-1317-1" target="_blank">978-1-4020-1317-1</a> <a href="#fnref:11" class="footnote-back-ref">↩</a></p></li> <li id="fn:12"><p>Gieré, R.; Stille, Peter (2018). Energy, Waste and the Environment: A Geochemical Perspective. Geological Society of London. p. 145. ISBN 978-1-86239-167-3. <a href="978-1-86239-167-3" target="_blank">978-1-86239-167-3</a> <a href="#fnref:12" class="footnote-back-ref">↩</a></p></li> <li id="fn:13"><p>Emergency Preparedness for Nuclear Powered Satellites. Stockholm: Organisation for Economic Co-operation and Development. 1990. p. 21. ISBN 9264133526. <a href="9264133526" target="_blank">9264133526</a> <a href="#fnref:13" class="footnote-back-ref">↩</a></p></li> <li id="fn:14"><p>Hardy, E. P.; Krey, P. W. & Volchock, H. L. (1972). Global inventory and distribution of Pu-238 from SNAP-9A (PDF). United States Atomic Energy Commission. p. 6. doi:10.2172/4689831. <a href="https://www.osti.gov/bridge/servlets/purl/4689831/4689831.pdf" target="_blank">https://www.osti.gov/bridge/servlets/purl/4689831/4689831.pdf</a> <a href="#fnref:14" class="footnote-back-ref">↩</a></p></li> <li id="fn:15"><p>SNAP-11 Surveyor Program, Third Quarterly Report <a href="https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19740074716_1974074716.pdf" target="_blank">https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19740074716_1974074716.pdf</a> <a href="#fnref:15" class="footnote-back-ref">↩</a></p></li> <li id="fn:16"><p>SNAP-11 Surveyor Program, Thirteenth Quarterly Report <a href="https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19740074787_1974074787.pdf" target="_blank">https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19740074787_1974074787.pdf</a> <a href="#fnref:16" class="footnote-back-ref">↩</a></p></li> <li id="fn:17"><p>SNAP 11 program. Final summary report, February 1962--January 1967 (Report). Martin Marietta Corp., Baltimore, Md. (USA). 1967-05-01. doi:10.2172/4219712. During the course of the SNAP 11 program, however, the application of this generator in the Surveyor mission was deleted. <a href="https://www.osti.gov/biblio/4219712" target="_blank">https://www.osti.gov/biblio/4219712</a> <a href="#fnref:17" class="footnote-back-ref">↩</a></p></li> <li id="fn:18"><p>SNAP-11 Surveyor Program, Thirteenth Quarterly Report <a href="https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19740074787_1974074787.pdf" target="_blank">https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19740074787_1974074787.pdf</a> <a href="#fnref:18" class="footnote-back-ref">↩</a></p></li> <li id="fn:19"><p>Fihelly, Arthur W.; Baxter, Charles F. (April 16, 1970). "The SNAP-19 Radioisotopic Thermoelectric Generator Experiment". IEEE Transactions on Geoscience Electronics. 8 (4): 255. Bibcode:1970ITGE....8..255F. doi:10.1109/TGE.1970.271419. <a href="https://doi.org/10.1109%2FTGE.1970.271419" target="_blank">https://doi.org/10.1109%2FTGE.1970.271419</a> <a href="#fnref:19" class="footnote-back-ref">↩</a></p></li> <li id="fn:20"><p>SNAP 19 Radioisotope Power Supply: Operation and Maintenance. Technical Manual (Report). January 1, 1967. doi:10.2172/4513086. OSTI 4513086. <a href="/wiki/Doi_(identifier)" target="_blank">/wiki/Doi_(identifier)</a> <a href="#fnref:20" class="footnote-back-ref">↩</a></p></li> <li id="fn:21"><p>"Home". NASA Radioisotope Power Systems. Archived from the original on 7 August 2012. Retrieved 31 March 2018. <a href="https://web.archive.org/web/20120807005925/http://solarsystem.nasa.gov/rps/rtg.cfm" target="_blank">https://web.archive.org/web/20120807005925/http://solarsystem.nasa.gov/rps/rtg.cfm</a> <a href="#fnref:21" class="footnote-back-ref">↩</a></p></li> <li id="fn:22"><p>"SNAP-19: Pioneer F & G, Final Report], Teledyne Isotopes, 1973". Archived from the original on 1 April 2018. Retrieved 31 March 2018. <a href="https://web.archive.org/web/20180401075331/https://www.osti.gov/cgi-bin/display_accomp_bib?specfile=/web/osti/docs/accomplishments/opentext/accomplishments.p2w&act=recquery&index=1439480" target="_blank">https://web.archive.org/web/20180401075331/https://www.osti.gov/cgi-bin/display_accomp_bib?specfile=/web/osti/docs/accomplishments/opentext/accomplishments.p2w&act=recquery&index=1439480</a> <a href="#fnref:22" class="footnote-back-ref">↩</a></p></li> <li id="fn:23"><p>McGrew, J. W. (January 1, 1970). "Report on the Properties and Performance of Tags". Energy, Proceedings. 70 (2). Hinsdale, Ill.: American Nuclear Society: 15.31–3. OSTI 4620225 – via www.osti.gov. <a href="https://www.osti.gov/biblio/4620225" target="_blank">https://www.osti.gov/biblio/4620225</a> <a href="#fnref:23" class="footnote-back-ref">↩</a></p></li> <li id="fn:24"><p>"Legacy Power Systems | Power and Thermal Systems". NASA Radioisotope Power Systems. Retrieved 2021-02-12. <a href="https://rps.nasa.gov/power-and-thermal-systems/legacy-power-systems" target="_blank">https://rps.nasa.gov/power-and-thermal-systems/legacy-power-systems</a> <a href="#fnref:24" class="footnote-back-ref">↩</a></p></li> <li id="fn:25"><p>Desai, Shail (2017-05-07). "1965 Nanda Devi spy mission, the movie". mint. Retrieved 2021-02-12. <a href="https://www.livemint.com/Sundayapp/g1GCx9n5O83AqHI4ClJAZP/1965-Nanda-Devi-spy-mission-the-movie.html" target="_blank">https://www.livemint.com/Sundayapp/g1GCx9n5O83AqHI4ClJAZP/1965-Nanda-Devi-spy-mission-the-movie.html</a> <a href="#fnref:25" class="footnote-back-ref">↩</a></p></li> <li id="fn:26"><p>SNAP-21 Program, Phase II. Deap Sea Radioisotope -Fueled Thermoelectric Generator Power Supply System. Quarterly Report No. 9, July 1, 1968 – September 30, 1968. Quarterly Report No. 9, July 1, 1968 – September 30, 1968 (Report). 1 January 1968. doi:10.2172/4816023. OSTI 4816023. <a href="https://digital.library.unt.edu/ark:/67531/metadc1056685/" target="_blank">https://digital.library.unt.edu/ark:/67531/metadc1056685/</a> <a href="#fnref:26" class="footnote-back-ref">↩</a></p></li> <li id="fn:27"><p>"Anthropogenic Radioactivity: Major Plume Source Points – RADNET: Section 11". www.davistownmuseum.org. Retrieved 31 March 2018. <a href="http://www.davistownmuseum.org/cbm/Rad8f.html" target="_blank">http://www.davistownmuseum.org/cbm/Rad8f.html</a> <a href="#fnref:27" class="footnote-back-ref">↩</a></p></li> <li id="fn:28"><p>Mandelberg, M. (1971). "An oceanographic acoustic beacon and data telemetry system powered by a SNAP-21 radiosotope thermoelectric generator". IEEE 1971 Conference on Engineering in the Ocean Environment. pp. 220–223. doi:10.1109/OCEANS.1971.1161004. <a href="/wiki/Doi_(identifier)" target="_blank">/wiki/Doi_(identifier)</a> <a href="#fnref:28" class="footnote-back-ref">↩</a></p></li> <li id="fn:29"><p>"Nuclear Batteries: Tools for Space Science - Atomic Insights". atomicinsights.com. September 1996. <a href="https://atomicinsights.com/nuclear-batteries-tools-for-space-science/" target="_blank">https://atomicinsights.com/nuclear-batteries-tools-for-space-science/</a> <a href="#fnref:29" class="footnote-back-ref">↩</a></p></li> <li id="fn:30"><p>Apollo 12 ALSEP Off-load transcript, containing comment about re-entry survivability of fuel cask <a href="https://history.nasa.gov/alsj/a12/a12.alsepoff.html" target="_blank">https://history.nasa.gov/alsj/a12/a12.alsepoff.html</a> <a href="#fnref:30" class="footnote-back-ref">↩</a></p></li> <li id="fn:31"><p>Space FAQ 10/13 – Controversial Questions, faq.org <a href="http://www.faqs.org/faqs/space/controversy/" target="_blank">http://www.faqs.org/faqs/space/controversy/</a> <a href="#fnref:31" class="footnote-back-ref">↩</a></p></li> <li id="fn:32"><p>Berry, E. R. (1963). "A GENERALIZED SHIELDING STUDY FOR NUCLEAR ELECTRIC SPACE POWER PLANTS". osti.gov. doi:10.2172/4005255. Retrieved 31 May 2024. <a href="https://doi.org/10.2172/4005255" target="_blank">https://doi.org/10.2172/4005255</a> <a href="#fnref:32" class="footnote-back-ref">↩</a></p></li> <li id="fn:33"><p>Aerojet General Corporation (November 1971). SNAP-8 Electrical generating system development program. NASA Lewis Research Center, Cleveland, Ohio. NASA CR-1907. <a href="#fnref:33" class="footnote-back-ref">↩</a></p></li> <li id="fn:34"><p>Voss, Susan (August 1984). SNAP Reactor Overview (PDF). Kirtland AFB, New Mexico: U.S. Air Force Weapons Laboratory. AFWL-TN-84-14. Archived (PDF) from the original on February 15, 2017. <a href="http://apps.dtic.mil/dtic/tr/fulltext/u2/a146831.pdf" target="_blank">http://apps.dtic.mil/dtic/tr/fulltext/u2/a146831.pdf</a> <a href="#fnref:34" class="footnote-back-ref">↩</a></p></li> <li id="fn:35"><p>SNAPSHOT, NASA Glenn Research Center, March 20, 2007. Retrieved 3 April 2019. <a href="https://web.archive.org/web/20030111163512/http://www.grc.nasa.gov/WWW/ion/past/60s/snapshot.htm" target="_blank">https://web.archive.org/web/20030111163512/http://www.grc.nasa.gov/WWW/ion/past/60s/snapshot.htm</a> <a href="#fnref:35" class="footnote-back-ref">↩</a></p></li> <li id="fn:36"><p>Snapshot, Gunther's Space Page. Retrieved 3 April 2019. <a href="https://space.skyrocket.de/doc_sdat/snapshot.htm" target="_blank">https://space.skyrocket.de/doc_sdat/snapshot.htm</a> <a href="#fnref:36" class="footnote-back-ref">↩</a></p></li> <li id="fn:37"><p>Voss, Susan (August 1984). SNAP Reactor Overview (PDF). Kirtland AFB, New Mexico: U.S. Air Force Weapons Laboratory. AFWL-TN-84-14. Archived (PDF) from the original on February 15, 2017. <a href="http://apps.dtic.mil/dtic/tr/fulltext/u2/a146831.pdf" target="_blank">http://apps.dtic.mil/dtic/tr/fulltext/u2/a146831.pdf</a> <a href="#fnref:37" class="footnote-back-ref">↩</a></p></li> </ol>