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Design of a deployable antenna system for a CubeSat, after investigating of various alternatives. The pin mechanism selected includes bases to attach the antennas and pins to wrap them around. The pins and bases are attached to the solar panels with small screws. The cables are routed to a connector
386:(USB) port and external power supply connector. Also an interface to MHX series radio modems from Microhard Systems is available on the flight module. The FM430 is equipped with an MSP430F1611 microcontroller, a 16 bit 8 MHz low power microcontroller from
615:
magnet. The magnetometer will help to counter the inherent bias and drifts of inertial sensors and provide measurement updates for a filtered and corrected solution of the attitude. The analog-digital conversion of all the sensor outputs is done by a
390:. It has many peripherals such as I2C (Inter-Integrated Communication), SPI (Serial Peripheral Interface), UART (Universal Asynchronous Receiver/Transmitter) buses, and also supports DMA (Direct Memory Access). It has a flash memory of 55
433:
In addition, ITUpSat-1 features a beacon for easy identification and continuous reporting of critical telemetry. Unlike the other transceiver, it always be on during the orbit, and be transmitting identification and simple telemetry in
660:
was built at the ITU for the operations (monitoring and control services) of ITUpSat-1. The MHX modem (Microhard
Systems) is also installed in the ground station for communication with the satellite's nominal communication system.
636:
with a detector array of 640 x 480 pixels (COTS imager based on the OV7620 image sensor). The objective is to take snapshot imagery. An interface board is designed to integrate camera with the MSP430F1611 microcontroller.
442:) every two minutes. This means anyone with the knowledge of the orbital parameters (in particular the amateur radio community) can easily pick up the satellite's signal. The beacon has a 100 mW RF output capacity.
365:
The electrical power subsystem consists of face-mounted solar panels, a regulator board and associated batteries. The system is able to charge itself (maximum power point tracking) and provide a regulated 3.3
319:
in India, and became the first
Turkish university satellite to orbit the Earth. It was expected to have a minimum of six-month life term, but it is still functioning for over two years. It is a
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1977:
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material (CubeSat Kit by
Pumpkin Inc.). There are three identical side faces and one face with access ports. The spacecraft stabilisation concept is discussed under Payload.
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2206:
1894:
796:
326:
The overall objectives are to provide a hands-on project environment for the students at the ITU under faculty guidance. The mission goals are to capture imagery of the
517:
382:
The FM430 flight module of
Pumpkin Inc. is being used. The FM430 is a compact solution for harsh environment systems. It has an SD (Secure Digital) card interface, one
2506:
2211:
1848:
1621:
2236:
2131:
458:, Germany) is being used to deploy the four CubeSats. The launch service interface for all CubeSats is provided by ISIS (Innovative Solutions In Space BV) from
410:
The primary on-board communication system is the MHX-425 transceiver from
Microhard Systems. This frequency hopping spread spectrum radio, which works in the
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2013:
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This subsystem represents the attitude sensing and passive stability hardware. It consists of three gyros, a three-axis accelerometer both from
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454:(launch provider: Antrix Corporation). The SPL (Single Picosatellite Launcher) system of Astrofein (Astro und Feinwerktechnik Adlershof GmbH,
430:
modulation), the data rate is 19.2 kbit/s. The transceiver interfaces directly to the on-board computer, it has a mass of about 80 gram.
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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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of ISRO (Indian Space
Research Organisation) with a launch mass of 960 kg. Further secondary payloads on this flight were:
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Launches are separated by dots ( • ), payloads by commas ( , ), multiple names for the same satellite by slashes ( / ).
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microprocessor which also has the task of grouping the measurements into a packet and sending them over the
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with side lengths of 10 centimetres (3.9 in) and a mass of 0.990 kilograms (2.18 lb).
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ITUpSat-1 was launched on 23 September 2009 as a secondary payload atop a PSLV launcher of
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payload, and to study the behavior of the passive stabilisation system of the CubeSat.
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648:) modes, transfer images in 8/16 bit modes and can be controlled over the I²C bus.
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representing the uppermost circuit of the electronics stack of the satellite.
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The CubeSat features two payloads. The first one is a sensor suite with an
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98.50 minutes, the local equatorial crossing time is at 12:00 hours.
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481:) on the east coast of India. The primary payload on the flight was
492:(Berlin Experimental Educational Satellite), a CubeSat of the TUB (
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near circular orbit at altitude of 720 kilometres (450 mi),
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band has adjustable hopping patterns, a high sensitivity (-115
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The spacecraft structure was purchased from
Pumpkin Inc. of
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bus to the on-board computer for downlink transmission.
2195:
Center for
Satellite Communications and Remote Sensing
770:İTÜ Uçak ve Uzay Bilimleri Fakültesi TA1KS ITUPSAT-1
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506:(University of Würzburg Experimentalsatellit-2),
2207:National Center for High Performance Computing
761:, ITU Space Systems Design and Test Laboratory
303:. It was launched on 23 September 2009 atop a
1971:
1849:BKZS (Regional Positioning and Timing System)
1615:
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289:Istanbul Technical University picoSatellite-1
8:
21:
2212:TRIGA Mark-II Training and Research Reactor
2003:
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607:in addition to a three-axis magnetometer (
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640:The camera can be operated in VGA/QVGA (
518:École Polytechnique Fédérale de Lausanne
398:. The microcontroller unit consumes 100
374:outside for connection to the antennas.
698:
297:Faculty of Aeronautics and Astronautics
45:Faculty of Aeronautics and Astronautics
2507:Earth observation satellites of Turkey
2160:Earth Sciences (Eurasia Institute of)
7:
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2172:Advanced Studies in Music Department
93:http://usl.itu.edu.tr/usl.itu.edu.tr
2512:Spacecraft launched by PSLV rockets
2202:Fuat Kulunk High Voltage Laboratory
2363:ITU Hornets American football team
2331:Natural History and Science Museum
186:Indian Space Research Organisation
14:
2137:Turkish Music State Conservatory
2102:Naval Architecture and Ocean Eng.
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2322:Suleyman Demirel Cultural Center
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2132:Textile Technologies and Design
2034:Chemical and Metallurgical Eng.
632:Payload #2 is a low-resolution
591:and are physically on the same
418:), and output power of up to 1
2057:Electrical and Electronic Eng.
730:"İstanbul Teknik Üniversitesi"
687:Polar Satellite Launch Vehicle
307:satellite launch vehicle from
78:
1:
2487:Istanbul Technical University
2252:Mühendishane-i Berr-i Hümayun
2247:Mühendishane-i Bahr-i Hümayun
2042:Computer and Informatics Eng.
1988:Istanbul Technical University
494:Technische Universität Berlin
301:Istanbul Technical University
49:Istanbul Technical University
646:Quarter Video Graphics Array
2502:Spacecraft launched in 2009
587:. The two payloads share a
2528:
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475:Satish Dhawan Space Centre
361:Electrical power subsystem
309:Satish Dhawan Space Centre
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2125: T
2111: S
2095: N
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2007: A
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16:Turkish CubeSat satellite
1910:Roketsan Research Center
1339:Universitetsky-Tatyana-2
2262:Yüksek Mühendis Mektebi
2259:Mühendis Mekteb-i Alisi
1631:Space program of Turkey
710:. Jonathan's Space Page
465:The launch site is the
2394:ITU in popular culture
2388:ITU Alumni Association
2169:Science and Technology
370:and 5 V bus service.
205:Reference system
115:Spacecraft properties
2327:Mustafa Inan Library
813:Orbital launches in
706:McDowell, Jonathan.
642:Video Graphics Array
384:Universal Serial Bus
2359:ITU basketball team
2117:Science and Letters
1944:Turksat (satellite)
736:on 21 February 2010
708:"Satellite Catalog"
23:
2492:Student satellites
2198:Central Laboratory
679:Spaceflight portal
534:nanosatellites of
402:of power at most.
394:and 10 kB of
270:23 September 2009
200:Orbital parameters
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2256:Hendese-i Mülkiye
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1940:Türksat (company)
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1766:Earth observation
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571:Sensor complement
406:RF communications
388:Texas Instruments
378:On-board computer
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152:23 September 2009
35:Earth observation
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2281:Ayazağa (Maslak)
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1001:Kwangmyŏngsŏng-2
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765:ITUpSAT1 Gallery
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732:. Archived from
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226:Perigee altitude
144:Start of mission
99:Mission duration
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1466:Progress M-MIM2
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589:microcontroller
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552:Sun-synchronous
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236:Apogee altitude
219:Sun-synchronous
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658:ground station
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1998:Undergraduate
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1925:Fergani Space
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1674:Communication
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1331:SumbandilaSat
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1319:Meteor-M No.1
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1309:USA-207 / PAN
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1287:Leonardo MPLM
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1216:Progress M-67
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1211:Sterkh No.11L
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340:San Francisco
333:
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295:built by the
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25:
19:
2428:
2019:Architecture
1885:TÜBİTAK UZAY
1878:Institutions
1653:
1589:
1571:Soyuz TMA-17
1569:
1480:
1396:Soyuz TMA-16
1394:
1368:
1280:
1178:
1104:Soyuz TMA-15
1102:
1055:
991:Eutelsat W2A
974:Soyuz TMA-14
972:
950:
898:Ekspress-MD1
740:24 September
738:. Retrieved
734:the original
724:
712:. Retrieved
701:
655:
639:
631:
602:
581:magnetometer
574:
550:
464:
449:
432:
409:
381:
372:
364:
337:
325:
288:
287:, short for
284:
283:
123:Pumpkin Inc.
120:Manufacturer
31:Mission type
18:
2419:MV Akdeniz
2166:Informatics
1842:In research
1551:Kosmos 2458
1547:Kosmos 2457
1543:Kosmos 2456
1517:Intelsat 15
1507:Eutelsat W7
1502:Intelsat 14
1497:Kosmos 2455
1422:WorldView-2
1390:STSS-Demo 2
1382:STSS-Demo 1
1373:SwissCube-1
1241:AprizeSat-4
1237:AprizeSat-3
1207:Kosmos 2454
1169:Kosmos 2453
1165:Kosmos 2452
1161:Kosmos 2451
1156:TerreStar-1
1140:Sirius FM-5
1072:ProtoStar 2
1030:Kosmos 2450
925:Telstar 11N
903:Hot Bird 10
634:CMOS camera
585:CMOS imager
558:is 98.28°,
556:inclination
479:Sriharikota
313:Sriharikota
246:Inclination
168:Launch site
149:Launch date
128:Launch mass
2481:Categories
2072:Management
2038:Civil Eng.
1938:See also:
1638:Satellites
1577:DirecTV-12
1565:Helios IIB
1417:COMSATBw-1
1413:Amazonas-2
1349:Oceansat-2
1233:Nanosat-1B
1221:DubaiSat-1
1189:AggieSat 2
1098:Meridian 2
1085:AeroCube-3
1006:Compass-G2
693:References
628:Payload #2
611:), and an
599:Payload #1
542:, Germany.
536:OHB-System
483:Oceansat-2
440:Morse code
344:California
334:Spacecraft
209:Geocentric
182:Contractor
2403:Radio ITU
2315:Buildings
2286:Gümüşsuyu
2014:AeroAstro
1560:Xi Wang 1
1491:ExPRESS-2
1487:ExPRESS-1
1369:ITU-pSat1
1357:Rubin 9.2
1353:Rubin 9.1
1302:September
1257:AsiaSat 5
1130:MEASAT-3a
1089:HawkSat-1
1081:PharmaSat
1020:SICRAL 1B
915:Spirale-B
911:Spirale-A
609:Honeywell
532:Rubin-9.2
528:Rubin-9.1
514:SwissCube
510:, Germany
500:, Germany
422:(437.325
348:aluminium
62:2009-051E
56:COSPAR ID
2497:CubeSats
2453:Category
2429:ITUpSAT1
2377:Arıyorum
2306:ITU-TRNC
2291:Taşkışla
2272:Campuses
2182:Research
2152:Graduate
2076:Maritime
1827:Göktürk
1801:Göktürk
1774:BILSAT-1
1739:Connecta
1664:UBAKUSAT
1654:ITUpSAT1
1556:Yaogan 8
1538:Yaogan 7
1526:December
1450:November
1361:BeeSat-1
1335:UGATUSAT
1327:Sterkh-2
1293:Palapa-D
1276:STSat-2A
1271:Optus D3
1267:JCSAT-RA
1229:UK-DMC 2
1225:Deimos-1
1174:RazakSAT
1077:TacSat-3
1063:Herschel
1025:Yaogan 6
930:Raduga-1
872:February
759:ITUpSAT1
665:See also
566:Payloads
522:Lausanne
508:Würzburg
490:BeeSat-1
305:PSLV-C14
285:ITUpSAT1
240:721.0 km
230:712.0 km
102:6 months
41:Operator
22:ITUpSAT1
2465:Commons
2391:ITU Day
2380:ITUFEST
2340:Stadium
2242:Faculty
2237:Rectors
2223:History
1900:Türksat
1682:Türksat
1646:Student
1533:USA-211
1482:STS-129
1461:PROBA-2
1432:USA-210
1406:October
1386:USA-209
1378:USA-208
1344:Nimiq 5
1282:STS-128
1262:USA-206
1180:STS-127
1135:GOES 14
1057:STS-125
1046:USA-205
1011:RISAT-2
996:USA-204
968:USA-203
952:STS-119
884:NOAA-19
858:Sohla-1
841:Orion 6
837:USA-202
830:January
299:at the
293:CubeSat
89:Website
77:SATCAT
2398:ITU TV
2352:Sports
2232:Alumni
2163:Energy
1920:Plan-S
1915:DeltaV
1441:NSS-12
1437:Thor 6
1250:August
1201:Pollux
1197:Castor
1193:BEVO-1
1185:JEM-EF
1125:LCROSS
1067:Planck
1015:ANUSAT
957:ITS S6
946:Kepler
822:2010 →
807:← 2008
613:Alnico
579:and a
540:Bremen
498:Berlin
456:Berlin
446:Launch
438:(e.g.
256:Period
250:98.28°
215:Regime
157:Rocket
2384:ITURO
2301:Tuzla
2296:Maçka
2086:Mines
1890:TUSAŞ
1784:İMECE
1779:RASAT
1470:Poisk
1365:UWE-2
1323:BLITS
1314:HTV-1
984:April
939:March
907:NSS-9
854:SDS-1
850:Kukai
846:Ibuki
714:3 May
547:Orbit
504:UWE-2
460:Delft
266:Epoch
131:990 g
84:35935
1942:and
1895:USET
1755:T3.2
1752:T3.1
1749:T2.1
1746:T1.2
1743:T1.1
1457:SMOS
1149:July
1114:June
963:GOCE
879:Omid
815:2009
742:2009
716:2018
530:and
471:SHAR
467:SDSC
452:ISRO
428:GFSK
355:5052
353:and
351:6061
328:CMOS
163:-C14
161:PSLV
1905:TUA
1121:LRO
1093:CP6
1039:May
920:OCO
622:I²C
618:PIC
593:PCB
577:IMU
496:),
424:MHz
416:dBm
412:UHF
396:RAM
176:FLP
79:no.
2483::
1732:6A
1727:5B
1722:5A
1717:4B
1712:4A
1707:3A
1702:2A
1697:1C
1692:1B
1687:1A
1558:,
1549:,
1545:,
1489:,
1459:,
1439:,
1415:,
1388:/
1384:,
1380:/
1371:,
1367:,
1363:,
1359:,
1355:,
1351:,
1337:,
1333:,
1329:,
1325:,
1321:,
1269:,
1239:,
1235:,
1231:,
1227:,
1223:,
1209:,
1199:,
1195:,
1191:,
1187:,
1167:,
1163:,
1123:,
1091:,
1087:,
1083:,
1079:,
1065:,
1013:,
913:,
909:,
905:,
896:,
856:,
852:,
848:,
839:/
656:A
538:,
520:,
477:,
436:CW
426:,
400:mW
392:kB
342:,
315:,
311:,
174:,
47:,
1979:e
1972:t
1965:v
1831:3
1810:2
1805:1
1623:e
1616:t
1609:v
1493:)
1485:(
1472:)
1468:(
1289:)
1285:(
1203:)
1183:(
959:)
955:(
798:e
791:t
784:v
744:.
718:.
644:/
473:(
469:‐
420:W
368:V
Text is available under the Creative Commons Attribution-ShareAlike License. Additional terms may apply.