107:
87:
618:
50:
447:
2604:
253:
An alternative payload was devised but not implemented consisting on four additional experiments: GOYA (Gamma-ray burst
Observer Yearned-Always), SIXE (Spanish Italian X-ray Experiment), DOPA, XRASE. These experiments would be later projected for the Minisat 02 before the whole project was scrapped.
207:
to test and develop the nation's capabilities to produce and manage spacecraft. To this end, INTA teamed up with private enterprises and universities to acquire funds and resources. Nonetheless, emphasis was also put on keeping the costs to a minimum and to ensure affordability.
270:(able to allocate up to 300 kg of payload), small (about 1145 mm x 1005 mm x 1170 mm) and projected to have a service life of 4 to 5 years. The body ended up weighing 195 kg (100 kg structure and 95 kg of payload) and was shaped like a
211:
The initial program was supposed to involve at least four minisatellites (Minisat 1 to 4) but only
Minisat 01 was put into orbit. A second design, the Minisat 02, was developed and tested in 2001 but the mission was canceled and the satellite was scrapped by 2002.
861:
D. Garcia-Asensio, M. Perez-Ayucar, M. A. Serrano, "MINISAT 01, Concept and
Evolution in the Operations of a Successful Small Mission," Proceedings of the 18th International Symposium on Space Flight Dynamics (ESA SP-548), Munich, Germany, 11–15 Oct.
324:
to measure temperature and active internal heaters around experiments and battery to keep the temperature within operational ranges. The kinetic unit ensured the
Minisat 01 maintained a favorable position to maximize
783:
M. A. Garcia Primo, "Spanish MINISAT Program – Objectives and
Operational Results," Proceedings of the 4th International Symposium on Small Satellites Systems and Services, 14–18 Sept. 1998, Antibes Juan les Pins,
266:, who was in charge of developing the platform, and INTA, who mainly devised the different payload and experiment implementation. A great degree of emphasis was put on keeping cost down so the construction was
198:
was a satellite developed in Spain as a means to kickstart its space program. The project started in 1990 and was funded by both the Inter-Ministerial
Committee of Space Science and Technology (CICYT) and the
682:
and a very good efficiency-weight ratio. Originally, 100 such detectors were to form the LEGRI sensing sub-unit but the experimental nature of this technology made INTA choose to mix an array of 80 HgI
320:
while managing the control subsystem. This was divided in two basic units: the thermal and the kinetic units. The first consisted of insulator coating around the body with both, internal and external,
601:
During its operational run, the liquid bridge would be oriented perpendicular to the z-axis (Sun-to-satellite direction) and activated for 5 minutes once a week. As a result, the satellite would
203:(INTA) who was also responsible for the project's management. After some feasibility studies, the satellite entered the design phase in 1993. The main objectives of the program were to develop a
1095:
Sanz-Andrés, Rodríguez-De-Francisco, Santiago-Prowald, Ángel , Pablo, Julián (2001). "The
Experiment CPLM (Comportamiento De Puentes Líquidos En Microgravedad) On Board MINISAT-01".
768:, responsible for maintaining the system's integrity until the firing of a pyro-kintetic charge which would signal the conditions were met to begin the whole placement process.
531:) to protect the measuring instruments. Under the grating, the Multi-Channel Plate (MCP) detectors with wedge and strip encoding are allocated, facing the exterior through a
1061:
Morales, Carmen; Trapero, Joaquín; Gómez, Jose F.; Orozco, Verónica; Giménez, Álvaro; Bowyer, Stuart; Edelstein, Jerry; Korpela, Eric; Lampton, Michael; Cobb, Jeff (2001).
713:
plate which is allocated in front of the detectors, a high voltage power supply needed to feed the device, and a processing unit which manages data and provides continuous
1717:
1238:
1130:
1622:
200:
67:
871:
Giménez, Álvaro. Science with
Minisat 01: Proceedings of the Workshop held in Madrid 26–28 April 1999. Dordrecht; Boston: Kluwer Academic Publishers, 2001.
907:
539:
and four possible positions. These were: open (transmitting all wavelength), shielded (blocks all emission and allows for internal radiation readings),
761:, gyro angle, and rate of the arm providing real-time corrections for the system and allowing a maximum deployment speed of 180º in about 3 minutes.
1570:
753:
was added to the end of a deploying arm directly connected to the gearbox. To ensure the correct positioning of the movable arm an electromagnetic
512:
nature of EUV, thus, ensuring a higher degree of precision. Each spectrometer was about 40x40x13 cm in size and 11 kg in weight with acute
1710:
550:
The device was placed at one end of the satellite, facing an anti-sun direction and it was operated continuously during the satellite's life.
2624:
1231:
2431:
462:
1703:
1144:
Suso, Julia; Blay, Pere; Almudena, Robert; Reglero, Victor; Eyles, Chris J. (2001). "LEGRI instrument health. A historical review".
574:, which were capable of measuring changes in position and shape of the fluid, and a command unit. This unit was itself built with a
737:
capable of deploying various devices such as solar panels, antennas, and proves. It consisted of an electrical motor connected a
582:
which measured the forces acting on the test fluid. The module was allocated inside a cylindrical container which also held the
1224:
329:
incidence on the solar panels in addition to stabilize the spacecraft on its 3 axis. This unit consisted on a combination of 3
881:
626:
559:
401:
31:
1004:
2144:
497:
2594:
2629:
1617:
977:
305:
1627:
714:
281:(550 mm x 800 mm in size) capable each to fully provide the power needed to run the satellite (about 50 W).
263:
285:
1180:
1952:
501:
278:
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718:
634:
381:
204:
95:
74:
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377:
365:
317:
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349:
which, working in cooperation, could provide accurate information on the satellite's position up to ±3º of
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687:
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707:
420:
313:
297:
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341:
in the spin plane. Data of the current position of the body was provided by two perpendicularly put
106:
2164:
2159:
1742:
1731:
1727:
1585:
1390:
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722:
690:
detectors. This decision also allowed them to directly compare their performance when working on a
678:(CIEMAT) capable of providing accurate readings on the operating energy range and a high degree of
645:
641:
567:
505:
470:
426:
After 5 years of successful operation, the satellite reentered the atmosphere on 14 February 2002.
2577:
Payloads are separated by bullets ( · ), launches by pipes ( | ). Crewed flights are indicated in
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1993:
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1914:
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fluxes. Besides the sensing sub-unit, LEGRI incorporated a filtering unit made of a mechanical
274:
with the experiments attacked to the top and bottom faces while the sides mounted 4 deployable
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734:
221:
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1859:
547:), and aluminum filter (which blocks most of the Lyman radiation while letting EUV through).
2320:
1958:
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1161:
1157:
1112:
1108:
1077:
699:
477:'s composition. The focus of these observations were oxygen lines and high energy (above 10
429:
During its whole service life it was operated by INTA, who monitored the satellite from the
412:
275:
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capable of regulating motion and providing a certain degree of stability. To simulate
2618:
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2276:
2035:
1968:
1864:
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1554:
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571:
536:
450:
416:
334:
837:
570:. It consisted of a test cell containing the fluid bridges embedded between several
316:. A bus connection links the microprocessor to the experiments capable of providing
2561:
2516:
2290:
2023:
1837:
1342:
661:
644:
capable of detecting low energy radiation (between 10 and 200 keV) produced by the
609:
longitudinally as a direct consequence from the accelerations applied at the CPLM.
583:
544:
517:
493:
478:
466:
346:
330:
309:
578:, able to change the direction of the bridges and to reset the experiment, and an
667:
The device was to incorporate some cutting-edge technology for its time, such as
2104:
2081:
2070:
1934:
1869:
1827:
1779:
1684:
1337:
1332:
1327:
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1302:
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446:
289:
17:
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1116:
1081:
703:
695:
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267:
160:
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234:
Espectrógrafo
Ultravioleta extremo para la observación de la Radiación Difusa
2451:
2351:
2310:
2075:
1963:
1919:
1874:
1773:
1762:
1643:
764:
The time control during the different phases of deployment was ensured by a
649:
638:
908:"El lanzamiento del satélite Minisat 01 desde Gran Canaria cumple 16 años"
2456:
2446:
2404:
1973:
1894:
1668:
1663:
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1491:
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1446:
1378:
1373:
1317:
1274:
1268:
1216:
758:
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710:
602:
482:
454:
326:
293:
2325:
2109:
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1983:
1899:
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1832:
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1503:
1439:
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1406:
1035:
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2240:
2088:
2029:
1940:
1853:
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361:
301:
2585:. Payloads deployed from other spacecraft are denoted in (brackets).
2229:
2179:
2154:
2099:
1792:
1768:
1451:
1063:"EURD: The Mission and the Stellar Absolute Fluxes OFB-type Stars"
625:
The LEGRI was developed by an international composed by INTA, the
616:
525:
445:
397:
393:
350:
288:
and the onboard central computing and processing unit (a modified
566:
when allocated inside axis-symmetric bridges under conditions of
532:
392:
21 April 1997. It was successfully put on a near-circular close
32:
Boolean satisfiability problem § Algorithms for solving SAT
1699:
1220:
400:
and 566 km of periapsis with and inclination of 151º (29º
236:– Extreme UV Spectrograph for the Study of Diffuse Radiation).
368:
speed of 1 Mbit/s and an uplink speed of 2 kbit/s.
30:
This article is about the satellite. For the SAT solver, see
356:
Communication with Earth was maintained using bidirectional
411:
The mission included the launch of the cremated remains of
562:
the CPLM was experimentation module created to study the
676:
1208:
795:"MINISAT-01 – eoPortal Directory – Satellite Missions"
500:(between 350 and 1100 Å). This allowed to compare and
461:
Being the result of the joint efforts of INTA and the
228:
in addition to four different scientific experiments:
2592:
520:
with holographically ruled 2460 lines/mm and made of
492:
To achieve that, the device employed two independent
621:
Fermi gamma telescope which is similar to the LEGRI.
247:
Experiencia Tecnológica de un Regulador de Velocidad
1677:
1636:
1610:
1594:
1547:
1512:
1471:
1464:
1399:
1363:
1261:
1254:
174:
156:
151:
135:
130:
114:
94:
73:
63:
457:were Lyman-alpha series is observable to the left.
239:CPLM (Column of Liquid Bridge in Microgravity).
2581:. Uncatalogued launch failures are listed in
1711:
1232:
8:
1129:: CS1 maint: multiple names: authors list (
42:
249:– Speed Regulator Technology Demonstrator).
1718:
1704:
1696:
1623:Instituto Nacional de Técnica Aeroespacial
1468:
1258:
1239:
1225:
1217:
473:in the interstellar medium to examine the
201:Instituto Nacional de Técnica Aeroespacial
105:
85:
48:
41:
1571:Madrid Deep Space Communications Complex
882:"Minisat-01. El primer satélite español"
220:The Minisat 01 was conceived to perform
2599:
1084:– via Kluwer Academic Publishers.
776:
1122:
516:(8 cm of diameter, 18 cm of
376:The S/C was launched from an American
888:(in European Spanish). 26 August 2012
423:along with those of 21 other people.
7:
1602:PLD Space Propulsion Test Facilities
674:emerging detectors developed by the
652:emitted by celestial bodies such as
637:. The main objective was to build a
485:whose presence may be indicative of
242:LEGRI (Low Energy Gamma Ray Imager).
1181:"El Minisat, satélite 100% español"
686:20, more conventional and reliable
733:Developed by CASA, the ETRV was a
717:readings on the satellite to ease
535:which provides them with 26º x 8º
504:the readings obtained to minimize
463:University of California, Berkeley
25:
481:), high mean life (above 1024 s)
2602:
543:filter (which allows to measure
433:(15º 37' 45" W, 27º 45' 49" N).
378:Lockheed L-1011-385-1-15 TriStar
262:The satellite was built between
1179:jdelaciencia (21 April 2015).
1146:Astrophysics and Space Science
1097:Astrophysics and Space Science
1070:Astrophysics and Space Science
1003:Seligmann, Jean (5 May 1997).
627:Rutherford Appleton Laboratory
560:Technical University of Madrid
360:transmitters operating on the
97:
1:
465:, this device was to conduct
1628:Spanish Astrobiology Center
958:"Launching the Great Bird".
934:"INTERDIC Articulo. Minisat"
2625:Spacecraft launched in 1997
824:Image Processing Laboratory
545:Lyman-alpha spectral series
2651:
1034:Pascual (5 October 2016).
980:. Celestis. Archived from
735:speed regulation mechanism
29:
2575:
1750:
1637:Commercial space industry
1618:Agencia Espacial Española
1548:Tracking and launch sites
380:registered N140SC with a
318:point-to-point interfaces
188:
184:
179:
170:
166:
147:
143:
126:
122:
59:
47:
1400:Science & technology
694:environment and sharing
635:University of Birmingham
496:equipped with modulable
469:observations of diffuse
292:microprocessor) with 32
54:Minisat 01 mission patch
1166:10.1023/A:1011614921688
1158:2001Ap&SS.276..299S
1117:10.1023/A:1012011903516
1109:2001Ap&SS.276...97S
1082:10.1023/A:1011661323989
594:sensors, and a back-up
205:technology demonstrator
180:EURD, CPLM, LEGRI, ETRV
1248:Space program of Spain
799:directory.eoportal.org
631:University of Valencia
622:
458:
1187:(in European Spanish)
978:"The Founders Flight"
820:"The MINISAT Project"
620:
449:
284:The core contained a
131:Spacecraft properties
1734:Orbital launches in
719:image reconstruction
337:to each other and a
2630:Satellites of Spain
1586:Villafranca Station
886:GranCanariaSpotters
642:gamma-ray telescope
44:
1576:Maspalomas Station
1209:INTA Official Site
1185:Juan de la Ciencia
984:on 8 February 2014
966:(27): 5. May 1997.
912:www.laprovincia.es
842:space.skyrocket.de
680:thermal resistance
623:
564:behavior of fluids
541:magnesium fluoride
459:
431:Maspalomas Station
396:of 585 km of
306:MIPS of throughput
2590:
2589:
1693:
1692:
1543:
1542:
1460:
1459:
1364:Earth observation
960:Star Trek Monthly
572:optical detectors
558:Developed by the
506:systematic errors
421:Gerard K. O'Neill
404:) and an orbital
382:Pegasus-XL rocket
300:, 512 kb of
222:Earth observation
192:
191:
27:Spanish satellite
16:(Redirected from
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2607:
2606:
2605:
2598:
1739:
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1737:
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1706:
1697:
1649:Pangea Aerospace
1595:Other facilities
1581:Cebreros Station
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1011:. Archived from
1000:
994:
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938:www.interdic.net
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700:background noise
413:Gene Roddenberry
345:and two biaxial
308:, 32 MB of
152:Start of mission
115:Mission duration
110:
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83:
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21:
18:Draft:Minisat 01
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2635:INTA satellites
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2571:
1746:
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1654:Zero 2 Infinity
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1016:
1015:on 2 April 2015
1002:
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914:. 21 April 2013
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766:pyrotechnic nut
741:mounted over a
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721:while avoiding
706:supported on a
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650:gamma radiation
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272:hexagonal prism
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1307:4B (cancelled)
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1262:Communications
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1203:External links
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739:torsion spring
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508:caused by the
467:spectrographic
451:Spectral lines
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386:Gando Air Base
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2487:Progress M-37
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2277:Progress M-36
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2036:Progress M-35
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2017:
2015:
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1969:Inmarsat-3 F4
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662:neutron stars
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495:
494:spectrometers
490:
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471:EUV radiation
468:
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456:
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418:
417:Timothy Leary
414:
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347:magnetometers
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312:and multiple
311:
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78:
76:
72:
69:
66:
62:
58:
51:
46:
40:
37:
33:
19:
2582:
2578:
2562:Early Bird 1
2557:Orbcomm FM12
2552:Orbcomm FM11
2547:Orbcomm FM10
2517:Intelsat 804
2419:
2356:
2350:
2291:EchoStar III
2239:
2230:Intelsat 803
2087:
2080:
2028:
2024:Intelsat 802
1951:
1939:
1889:
1852:
1838:Intelsat 801
1823:Gonets-D1 #6
1818:Gonets-D1 #5
1813:Gonets-D1 #4
1785:
1778:
1761:
1754:
1611:Institutions
1411:
1212:(in Spanish)
1189:. Retrieved
1184:
1174:
1149:
1145:
1139:
1125:cite journal
1100:
1096:
1090:
1073:
1069:
1056:
1044:. Retrieved
1042:(in Spanish)
1039:
1036:"Minisat 01"
1029:
1017:. Retrieved
1013:the original
1008:
1005:"Ashes Away"
998:
986:. Retrieved
982:the original
972:
963:
959:
953:
941:. Retrieved
937:
928:
916:. Retrieved
911:
902:
890:. Retrieved
885:
876:
867:
857:
845:. Retrieved
841:
838:"Minisat 01"
832:
823:
814:
802:. Retrieved
798:
789:
779:
763:
732:
723:signal noise
675:
666:
658:binary stars
624:
600:
584:power supply
568:microgravity
557:
549:
518:focal length
491:
460:
428:
425:
410:
375:
355:
335:orthogonally
310:data storage
286:NiCd battery
283:
279:solar panels
261:
252:
246:
233:
219:
210:
195:
193:
38:
36:
2609:Spaceflight
2542:Orbcomm FM9
2537:Orbcomm FM8
2532:Orbcomm FM7
2527:Orbcomm FM6
2522:Orbcomm FM5
2482:Kosmos 2348
2477:Kosmos 2347
2426:SPARTAN-201
2220:Kosmos 2346
2105:Kosmos 2345
2094:CRISTA-SPAS
2082:Soyuz TM-26
2071:Superbird-C
1979:Kosmos 2344
1947:Kosmos 2343
1935:Kosmos 2342
1930:Chinasat 6A
1885:Kosmos 2341
1870:Kosmos 2340
1843:Mozhayets 2
1808:Kosmos 2339
1803:Kosmos 2338
1798:Kosmos 2337
1780:Soyuz TM-25
1685:Pedro Duque
1520:Capricornio
1280:Spainsat NG
1271:/ XTAR-LANT
1076:: 141–150.
755:Reed switch
654:black holes
629:(RAL), the
596:memory card
588:temperature
487:dark matter
437:Experiments
343:Sun sensors
331:torque rods
322:thermistors
290:Intel 80386
136:Launch mass
2619:Categories
2512:Iridium 49
2507:Iridium 48
2502:Iridium 47
2497:Iridium 46
2492:Iridium 45
2467:Iridium 44
2462:Iridium 42
2410:IndoStar-1
2395:Iridium 43
2390:Iridium 41
2385:Iridium 40
2380:Iridium 39
2375:Iridium 38
2331:FalconGOLD
2281:Sputnik 40
2267:Iridium 37
2262:Iridium 36
2257:Iridium 35
2252:Iridium 34
2247:Iridium 19
2215:Iridium 33
2210:Iridium 32
2205:Iridium 31
2200:Iridium 30
2195:Iridium 29
2190:Iridium 28
2185:Iridium 27
2175:Meteosat 7
2170:Hot Bird 3
2135:Iridium 26
2130:Iridium 25
2125:Iridium 24
2120:Iridium 23
2115:Iridium 22
2061:Iridium 21
2056:Iridium 20
2051:Iridium 18
2046:Iridium 17
2041:Iridium 15
2019:Iridium 16
2014:Iridium 14
2009:Iridium 13
2004:Iridium 12
1999:Iridium 11
1994:Iridium 10
1984:Fengyun 2A
1890:Minisat 01
1678:Astronauts
1659:Alén Space
1567:(proposed)
1472:Suborbital
1412:Minisat 01
1255:Satellites
772:References
749:, a small
704:collimator
646:dispersion
633:, and the
586:, several
475:Mesosphere
402:retrograde
196:Minisat 01
161:Pegasus-XL
43:Minisat 01
2579:underline
2567:AsiaSat 3
2472:Galaxy 8i
2452:Equator-S
2442:Hikoboshi
2352:VLS-1 V01
2311:Apstar 2R
2296:Foton #11
2225:FAISAT-2V
2076:OrbView-2
1989:Iridium 9
1964:Telstar 5
1953:Tselina-2
1925:Iridium 8
1920:Iridium 7
1915:Iridium 6
1910:Iridium 5
1905:Iridium 4
1875:Thaicom 3
1774:Nahuel 1A
1763:GPS IIR-1
1644:PLD Space
1565:El Hierro
1284:Amazonas
1040:EsasCosas
708:honeycomb
639:prototype
483:neutrinos
226:low orbit
81:1997-018A
75:COSPAR ID
2457:Astra 1G
2447:JCSAT-1B
2405:Sirius 2
2341:Maqsat-H
2336:Maqsat-B
1974:INSAT-2D
1895:Founders
1669:Hisdesat
1664:Hispasat
1525:Bloostar
1447:Xatcobeo
1431:UPM-Sat
1416:Nanosat
1318:Hispasat
1275:XTAR-EUR
1269:Spainsat
1019:22 March
1009:Newsweek
988:25 April
759:momentum
751:flywheel
747:payloads
715:attitude
711:tungsten
592:pressure
510:ionizing
455:Hydrogen
398:apoapsis
366:downlink
327:sunlight
64:Operator
2583:italics
2437:Orihime
2370:USA-136
2365:USA-134
2326:USA-135
2316:USA-133
2305:Huygens
2301:Cassini
2110:Agila 2
2066:USA-132
1900:GOES 10
1880:BSAT-1a
1860:USA-131
1848:Tempo-2
1833:USA-130
1828:JCSAT-R
1530:Miura 5
1513:Orbital
1504:Miura 1
1465:Rockets
1407:Intasat
1391:Ingenio
1370:Deimos
1154:Bibcode
1105:Bibcode
826:. 2010.
743:gearbox
605:±0.375
529:carbide
522:silicon
514:grating
388:in the
364:with a
333:placed
268:modular
216:Mission
175:Payload
118:5 years
96:SATCAT
2595:Portal
2421:STS-87
2358:SCD-2A
2321:STEP-4
2272:IRS-1D
2241:STS-86
2089:STS-85
2030:STS-94
1959:Thor 2
1941:STS-84
1854:STS-83
1793:Haruka
1787:STS-82
1756:STS-81
1743:1998 →
1728:← 1996
1355:Lume-1
784:France
688:CdZnTe
502:filter
406:period
372:Launch
362:S-band
304:, 2.4
302:EEPROM
245:ETRV (
232:EURD (
157:Rocket
139:195 kg
2400:Kupon
2285:X-Mir
2155:FORTE
2150:PAS-5
2140:Lewis
2100:PAS-6
1483:INTA
1452:OPTOS
1191:8 May
1066:(PDF)
1046:8 May
943:8 May
918:8 May
892:8 May
847:6 May
804:6 May
613:LEGRI
576:motor
526:boron
394:orbit
384:from
351:error
224:on a
103:24779
2432:TRMM
2180:GE-3
1769:GE 2
1736:1997
1535:Meso
1479:Argo
1193:2020
1131:link
1048:2020
1021:2015
990:2015
945:2020
920:2020
894:2020
862:2004
849:2020
806:2020
729:ETRV
698:and
603:spin
590:and
554:CPLM
533:lens
442:EURD
276:AsGa
264:CASA
258:Body
194:The
68:INTA
2346:YES
2283:,
2145:ACE
1497:300
1492:255
1487:100
1386:Paz
1343:AG1
1162:doi
1150:276
1113:doi
1101:276
1078:doi
1074:276
696:FEE
692:0 g
669:HgI
660:or
648:of
607:rpm
537:FOV
453:of
298:RAM
296:of
98:no.
2621::
1425:1B
1348:1F
1338:1D
1333:1C
1328:1B
1323:1A
1303:4A
1183:.
1160:.
1148:.
1127:}}
1123:{{
1111:.
1099:.
1072:.
1068:.
1038:.
1007:.
962:.
936:.
910:.
884:.
840:.
822:.
797:.
725:.
664:.
656:,
598:.
489:.
479:eV
419:,
415:,
358:RF
353:.
294:Mb
2597::
2428:)
2424:(
2361:)
2355:(
2307:)
2303:(
2287:)
2279:(
2096:)
2092:(
1719:e
1712:t
1705:v
1440:2
1435:1
1420:1
1379:2
1374:1
1311:5
1298:3
1293:2
1288:1
1240:e
1233:t
1226:v
1195:.
1168:.
1164::
1156::
1133:)
1119:.
1115::
1107::
1080::
1050:.
1023:.
992:.
964:1
947:.
922:.
896:.
851:.
808:.
684:2
671:2
524:/
34:.
20:)
Text is available under the Creative Commons Attribution-ShareAlike License. Additional terms may apply.
