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Radio Aurora Explorer

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instabilities can create magnetic field-aligned irregularities (FAI), which are dense plasma clouds known to disrupt communication between Earth and orbiting spacecraft. To study FAI, the RAX satellites utilize a large incoherent scatter radar located in Poker Flat, Alaska (known as PFISR). PFISR transmits powerful radio signals into the plasma instabilities, which then scatter in the FAI and are received by the orbiting RAX spacecraft. The signals are then processed by RAX's onboard computer and transmitted back to Earth for scientific analysis. Earth-based scientists have been unable to study these unique plasma formations from the ground, and RAX will serve as a key transition point between Earth and Space.
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CubeSat design, and was able to execute bistatic radar measurements never before been performed with such a spacecraft. RAX team members applied the lessons learned from RAX-1 to the design of a second flight unit, RAX-2, which will perform the same mission concept of the first RAX that launched in November 2010, with improved bus performance and additional operational modes. Science measurements will be enhanced through interactive experiments with high power ionospheric heaters where FAI will be generated on demand.
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experienced by the satellite throughout its orbit over time. The cage was designed to characterize the magnetometers and run hardware-in-the-loop testing with RAX. This essentially puts the CubeSat into a virtual orbit, and allows the team to generate appropriate magnetic fields to test RAX's ability
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The scientific payload and the majority of the bus systems performed as expected, including the GPS-based position and time subsystem, attitude determination and control, communications, and on-board processing. Unfortunately, the mission ended prematurely after approximately two months of operation
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The goal of the RAX-2 mission is to enhance understanding of FAI formation so that short-term forecast models can be generated. This will aid spacecraft operators with planning their mission operations around periods of expected communication disruption. The RAX-1 mission made great strides in
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RAX is capable of carrying out scientific procedures that previously could only be done with large satellites, thanks in part to new enabling technologies. RAX's primary mission objective is to study large plasma formations in the ionosphere, the highest region of our atmosphere. These plasma
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builds on this heritage by completing the scientific portion of the overall mission; it is a reflection of students learning from practical experience, and swiftly implementing new, more inventive technologies firsthand. RAX team members were able to get practical spacecraft troubleshooting
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RAX undergoes the same rigorous testing that its bigger cousins do, to meet many of the same requirements. During testing, RAX was able to successfully upload commands and receive telemetry from a host of sensors. These sensors yielded data including temperature and voltage,
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position and velocity, spacecraft attitude (for orientation determination), and the general status of all of the RAX subsystems. The ground station software was also tested over radio links, proving that the team will be able to listen and interact with RAX remotely.
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The RAX-1 mission, launched in November 2010, was a demonstration of the team's technological capabilities – it made great strides in CubeSat design, and was able to execute bistatic radar measurements that had never before been performed on a satellite of its size.
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experience, and applied lessons learned from RAX-1 to RAX-2, which performs the same mission concept with improved bus performance and additional operational modes. RAX-2 launched on October 28, 2011 as part of the NASA
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in California on a United Launch Alliance Delta II rocket, flying in the 7920-10 configuration. CubeSat separation occurred 98 minutes after launch, and beacons from RAX-2 were heard shortly thereafter.
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due to a gradual degradation of the solar panels that ultimately resulted in a loss of power. RAX team members applied the lessons learned from RAX-1 to the design of a second flight unit, RAX-2.
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Over the course of the seventeen-month development, the team also built additional testing facilities to evaluate sensors and prototypes. An in-house
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are underlined. Launch failures are marked with the † sign. Payloads deployed from other spacecraft are (enclosed in parentheses).
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to determine how it is oriented. The Helmholtz Cage is also used to evaluate magnetic cleanliness and final integration testing.
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Launches are separated by dots ( • ), payloads by commas ( , ), multiple names for the same satellite by slashes ( / ).
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RAX-1 was sent into orbit on November 19, 2010 by the United States Air Force as a payload manifested on the
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RAX Attitude Determination Presentation, University of Michigan Summer Undergraduate Research in Engineering
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mission. The CubeSat launch was sponsored by NASA as part of the ElaNA-3 program. It launched from
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RAX-2 launched on October 28, 2011, as a secondary payload on NASA's
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Cage was constructed to create and simulate the changes in
404:. There are currently two satellites in the RAX mission. 688: 685:"RAX-Radio Aurora Explorer Mission Science Operations" 743:"NASA - ELaNa: Educational Launch of Nanosatellites" 634:"NASA - ELaNa: Educational Launch of Nanosatellites" 1548: 1451: 1370: 1290: 1255: 1213: 1126: 1052: 985: 917: 875: 854: 767:"Tracking Station | Worldwide launch schedule" 388:mission. The RAX mission is a joint effort between 353: 343: 333: 323: 313: 303: 293: 283: 273: 263: 258: 235: 230: 212: 199: 189: 173: 168: 152: 142: 137: 111: 98: 77: 63: 55: 610:"NASA - Expendable Launch Vehicle Status Report" 482:mission, launched from Kodiak Launch Complex on 396:in Ann Arbor, Michigan. The chief scientist at 815: 8: 34: 822: 808: 800: 89: 40: 33: 27:"RAX" redirects here. For other uses, see 580:National Science Foundation Press Release 674:page at eoPortal (accessed Sept 15 2014) 552: 550: 548: 546: 544: 490:. The rocket used for this launch was a 1675:Spacecraft launched by Minotaur rockets 628: 626: 540: 494:rocket developed by Orbital Sciences. 7: 1149:Dragon Spacecraft Qualification Unit 473:United States Department of Defense 423:Capabilities and mission objectives 392:in Menlo Park, California and the 25: 708:NASA Goddard Spaceflight Center, 786: 755:from the original on 2023-06-15. 402:Michigan Exploration Laboratory 35:Radio Aurora Explorer (USA-218) 101: 1: 687:. Rax.sri.com. Archived from 156:28.0 kilograms (61.7 lb) 309:653 kilometres (406 mi) 299:622 kilometres (386 mi) 1670:Spacecraft launched in 2010 382:National Science Foundation 1701: 524:NPOESS Preparatory Project 510: 177:20 November 2010, 01:25:00 26: 1635: 1571:SpaceX COTS Demo Flight 1 528:Vandenberg Air Force Base 367: 363: 254: 250: 226: 222: 164: 160: 133: 129: 51: 39: 591:RAX-1 Mission Completed 561:. Jonathan's Space Page 1685:University of Michigan 636:. Nasa.gov. 2011-02-14 394:University of Michigan 46:RAX under construction 374:Radio Aurora Explorer 264:Reference system 138:Spacecraft properties 838:Orbital launches in 724:. Space.skyrocket.de 557:McDowell, Jonathan. 1505:USA-222 / FASTRAC-2 1501:USA-222 / FASTRAC-1 559:"Satellite Catalog" 349:311.60 degrees 345:Argument of perigee 181:2010-11-20UTC01:25Z 36: 1660:Student satellites 794:Spaceflight portal 659:2011-06-05 at the 596:2012-03-17 at the 476:Space Test Program 339:73.62 degrees 329:97.52 minutes 319:71.97 degrees 259:Orbital parameters 1680:SRI International 1647: 1646: 1516:USA-219 / O/OREOS 1483:USA-220 / FASTSAT 769:. 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Nasa.gov 535:References 384:sponsored 268:Geocentric 213:Contractor 147:3U CubeSat 1575:Mayflower 1378:Chang'e 2 1344:Yaogan 11 1334:Michibiki 1291:September 1272:Yaogan 10 1104:Negai ☆'' 1012:CryoSat-2 972:Yaogan 9C 968:Yaogan 9B 964:Yaogan 9A 951:GLONASS-M 940:GLONASS-M 929:GLONASS-M 478:’s (STP) 451:Helmholtz 289:0.0021634 278:Low Earth 185: UTC 85:2010-062B 79:COSPAR ID 1665:CubeSats 1549:December 1479:STPSat-2 1452:November 1316:Gonets-M 1238:AISSat-1 1230:AlSat-2A 1200:Chollian 1186:TanDEM-X 1155:STSAT-2B 1134:SERVIS-2 1109:Astra 3B 1076:Akatsuki 876:February 753:Archived 657:Archived 594:Archived 239:May 2011 64:Operator 1621:GSAT-5P 1540:HYLAS-1 1526:Orion 7 1522:USA-223 1493:USA-221 1469:COSMO-4 1438:BSat 3B 1371:October 1357:USA-216 1339:USA-215 1277:USA-214 1242:TIsat-1 1234:StudSat 1118:USA-213 1092:Shin'en 1070:ICC-VLD 1066:Rassvet 1061:STS-132 1029:USA-212 1001:STS-131 889:STS-130 855:January 498:Results 480:STP-S26 436:Testing 386:CubeSat 243:2011-06 241: ( 179: ( 112:Website 100:SATCAT 1627:KA-SAT 1318:No.2, 1256:August 1191:Ofek-9 1170:Picard 1166:Prisma 1144:Badr-5 1100:Hayato 1088:DCAM-2 1084:DCAM-1 1080:IKAROS 1018:GSAT-4 898:Cupola 847:2011 → 832:← 2009 518:Launch 488:Alaska 467:Launch 325:Period 274:Regime 204:Kodiak 190:Rocket 121:.umich 119:.engin 1587:QbX-2 1583:QbX-1 1174:BPA-1 1034:SES-1 986:April 918:March 672:RAX-2 565:3 May 513:RAX-2 417:ELaNa 412:RAX-2 355:Epoch 207:Pad 1 107:37223 1399:XM-5 1214:July 1127:June 840:2010 748:NASA 567:2018 335:RAAN 123:.edu 68:NASA 1491:), 1090:), 1053:May 954:735 943:732 932:731 904:SDO 486:in 443:GPS 378:RAX 117:rax 102:no. 72:NSF 29:Rax 18:RAX 1656:: 1601:, 1597:, 1593:, 1589:, 1585:, 1581:, 1577:, 1573:, 1563:, 1559:, 1538:, 1524:/ 1513:, 1507:, 1503:, 1499:, 1495:/ 1481:, 1436:, 1422:, 1418:, 1414:, 1410:, 1406:, 1385:, 1350:, 1346:, 1322:, 1304:, 1300:, 1265:, 1240:, 1236:, 1232:, 1228:, 1198:, 1172:, 1168:, 1111:, 1102:, 1098:, 1094:, 1086:, 1078:, 1068:, 970:, 966:, 949:/ 945:, 938:/ 934:, 927:/ 896:, 751:. 745:. 625:^ 543:^ 1485:( 1082:( 1072:) 1064:( 1008:) 1004:( 900:) 892:( 823:e 816:t 809:v 776:. 731:. 698:. 643:. 619:. 569:. 376:( 245:) 183:) 31:. 20:)

Index

RAX
Rax

NASA
NSF
COSPAR ID
2010-062B
Edit this at Wikidata
SATCAT no.
rax.engin.umich.edu
3U CubeSat
Minotaur IV/HAPS
Kodiak
Pad 1
Orbital Sciences
Geocentric
Low Earth
Eccentricity
Perigee altitude
Apogee altitude
Inclination
Period
RAAN
Argument of perigee
Epoch
National Science Foundation
CubeSat
SRI International
University of Michigan
SRI International

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