Спутник технологический. STRV 1C. [Редактировать]

КА STRV 1С и STRV 1D изготовлены Агентством оборонных оценок и исследований Министерства обороны Великобритании (Defense Evaluation and Research Agency, ранее именовалось RAE – Royal Aircraft Establishment) в рамках программы по исследованию космических технологий STRV (Space Technology Research Vehicle). КА имеют форму куба со стороной 0.7 м. КА на орбите стабилизируются вращением со скоростью 10° в секунду.

Дополнительные наименования

#НаименованияПоиск в новостяхПоиск в документах
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Дополнительная классификация

#Наименования
1Тип оператора(владельца) - военные
2Страна оператор(владелец) - Великобритания
3Страна производитель - Великобритания

Новостная лента[Найти информацию в новостях] [Найти информацию в документах]

#Новостная лента.
12001-01 - 2001-02. Аппарат потерянн вследствие ошибок в дизайнеТэги: STRV 1C

Технические характеристики

#ХарактеристикаЗначение
1Масса, кг104.0
2Габариты, метра0.7х0.7х0.7
3Мощность, Вт80

Пусковые характеристики

#ХарактеристикаЗначение
1Код NSSDC2000-072C

Информация об удачном запуске

#ХарактеристикаЗначение
1Космодром Космодром Куру
2Дата пуска2000-11-16 at 01:07:00 UTC
3Полезная нагрузка 1xPAS 1R
4Полезная нагрузка 1xAMSAT P3D
5Полезная нагрузка 1xSTRV 1C
6Полезная нагрузка 1xSTRV 1D
7Ракета-носитель 1xАриан 5G

Найдено 71 документов по запросу «STRV 1C». [Перейти к поиску]


Дата загрузки: 2017-10-09
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0.38/5
THE SPACE TECHNOLOGY RESEARCH VEHICLES : STRV-1A,B,C&D Cdr Richard Blott RN... Space Agency, is also discussed. STRV 1c&d are currently scheduled to launch... a nominal one year mission. Fig 1 STRV 1a and b 1. Introduction Abstract The... the Space Technology Research Vehicle (STRV) 1a&b microsatellite mission in geostationary... a short timescale. The followon mission : STRV 1c&d will also be designed and... payload, sponsored by the UK STRV 1a&b were designed with the... ground segment. Details of the STRV 1a&b mission were presented to... decided to contribute 3 experiments to STRV 1c&d. STRV 1c&d will also exploit the characteristics... Belts Atomic oxygen erosion Fig 2 STRV in GTO Schematic are being... of the STRV 1a&b experience. This paper addresses the STRV 1a&b performance... of 1996. Plans for the STRV 1c&d mission are then described with... and the associated design modifications. 2. STRV 1a&b - Second Year in Orbit.... During the long eclipse the STRV 1a&b battery anomaly, described in... the physical data links. The STRV spacecraft were the first in... hosted on one of the STRV 1b spacecraft Mil Std 1750A... code and debugged using an STRV engineering model. After debugging, the software was uploaded to STRV 1b with the assistance of... workstation which transmits them as STRV CCSDS packets to the spacecraft.... As a part of this experiment, STRV 1b was given its own... sites to an operational spacecraft. STRV 1b TC - 125bps TM - 1Kbps... follow-on missions. 4. STRV 1c&d Fig 7 STRV 1c and d The STRV 1c&d mission is now defined... have the same orbit as STRV 1a&b. The spacecraft and ground.... The first objective of the STRV programme is demonstrate the application..., following the success of the STRV 1b SCPS experiment, advantage will... Radiation Environment Monitor flown on STRV 1b complemented by devices to... Earth Sensor. Both underperformed in STRV 1a&b and although this did... solar aspect angle experienced on STRV 1a&b. Finally, there are a range..., integration and test of the STRV 1c&d spacecraft and experiment payload starts.... However, the lessons learned form STRV 1a&b indicate that there may... it is required. 5. Conclusions The STRV 1a&b mission has proved much... design of the follow on STRV 1c&d mission. It is also most... who participated in STRV 1a&b are flying experiments on STRV 1c&d and that... a space technology research vehicle with STRV 1a&b it is possible to..., achieved with STRV 1a&b, is being reduced to 2 years for STRV 1c&d. Although... gratefully received contributions of the STRV 1a&b and c&d project teams. The...(F) “The Space Technology Research Vehicle (STRV 1)”, Proc. Royal Aeronautical Society Conf...”, March 1993. 3. N. Wells et al “STRV-1a/b : The first Results”, Proc..., “The Space Technology Research Vehicles STRV -1A and -1B: One Year.... 8. Biography Mr. Wells is the STRV-1a/b Mission Manager in the... also the Spacecraft Manager for STRV-1b and is responsible for...-to-day operations of the STRV-1b spacecraft. Prior to launch... design and development of the STRV-1b and has been a member... BSc MIEE CEng is the STRV 1c&d Project Manager. He joined the...



Дата загрузки: 2017-06-15
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0.15/5
...THE SPACE TECHNOLOGY RESEARCH VEHICLES: STRV~ lA,B,C&D Cdr Richard Blott RN... Canadian Space Agency, is also STRV 1c&d are currently discussed. scheduled to... a nominal one year mission. Fig 1 STRV la and b 1. Introduction Abstract The... achievements of the Space Technology (STRV) 1a&b Research Vehicle micro sate... timescale. The follow-on mission : STRV Ic&d will also be designed..., the UK Particle Physics and STRV Ia&b were designed with the... Allen Belts Details of the STRV la&b mlSSIOn were presented to... orbit. Atomic oxygen erosion Fig 2 STRV in GTO Schematic are being... of the STRV 1a&b experience. This paper addresses the STRV la&b performance... of 1996. Plans for the STRV 1c&d mISSlOn are then described with... decided to contribute 3 experiments to STRV lc&d. 2. STRV la&b - Second Year in... then without eclipse, see figure 3. STRV 1c&d will also exploit the ch..., although payload 2 I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I Eclipse durations for STRV-1a and .1b Although the.... During the long eclipse the STRV la&b battery anomaly, described in...



Дата загрузки: 2017-06-15
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0.2/5
... Evaluation & Research Agency (DERA), called STRV-1c and –1d. Between them, these... Space Technology Research Vehicle microsatellites (STRV-1a and –1b), which were... 1994, the follow-on programme, STRV-1c & -1d, was initiated. During the... could be directly reused in STRV-1c/d. Clearly, the larger structure would... adopted from the basic STRV-1a/b design. Figure 1: STRV-1c/d on the ASAP... the ASAP-5 User’s Manual. 1 The STRV-1c/d development programme was occurring in... device supplied by Arianespace Figure 2: STRV-1c under vibration test Test Requirements... system was previously used on STRV-1a/b, however, they were not... Test Philosophy STRV-1c/d Power ACS The majority of the STRV-1c/d test programme... shear walls X Ground Station Centre 5 STRV Comm’s Simulator Tri-axis accelerometer... an almost identical manner, only STRV-1c data is considered. Figure 12... Xaxis random vibration test of STRV-1c. The dominant fundamental mode at... SSC00-I-7 Conclusions & The Future The STRV-1c & -1d spacecraft have successfully completed... of STRV-1c & -1d is awaited, plans are already underway for STRV-1e... to embark on the next STRV programme. The thermal models of...



Дата загрузки: 2017-10-09
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0.77/5
... the Space Technology Research Vehicle (STRV-1C) mission, to be launched in... will carry a microGPS, SNOE and STRV, the computer will be on..., as planned for SNOE and STRV) or processed in real or... <1 W at peak. B. STRV-1C Mission The Space Technology Research Vehicle (STRV-1C) is the...), STRV-1A and -1B were launched in June 1994, and STRV-1C is... receiver will be carried on STRV-1C, whose development is jointly sponsored... the DRA. The goal of STRV’s microGPS will be to characterize... of the Earth (relative to STRV) actually spills past the Earth’s limb and will illuminate STRV. In addition, because it is... platforms for the SNOE and STRV missions are ground-based Macintosh...



Дата загрузки: 2016-11-02
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0.04/5
... 5 de abril de 1967. DIADEME 1 D-1C 08.02.1967 Francia GEO....05.1985 Francia COM TELECOM 1C 11.03.1988 Francia COM... con el satélite ARABSAT-1C. Construido por la Space Systems... que también llevaba al FY-1C. Estuvo en una órbita de... Este. Se perdió contacto FY-1C 10.05.1999 China MET....05.2013 China COM ZHONGXING 1C 09.12.2015 China MIL... años. También llamado ZX-1C y Chinasat-1C. Satélite de telecomunicaciones, quiz....12.2000 China NAV BEIDOU 1C 24.05.2003 China NAV....2010 China EXP ZHEDA PIXING 1C 22.09.2010 China EXP... 2011-032A. También llamado TL-1C. Satélite de telecomunicaciones para... proyectada de 8 años. TIAN LIAN 1C 25.07.2012 China COM... 2008041B. También llamado HUAN JING 1C. Satélite de observación terrestre....09.2008 China APL HJ-1C 18.11.2012 China APL... de altura. También llamado TH-1C. Satélite de observación terrestre... 3 satélites (Fengniao1A y 1B y HJ-1C). Fue enviado a una órbita polar...én llevaba otros 3 satélites (HJ-1C, Fengniao-1B y Xinyan-1). Fue enviado...én llevaba otros 3 satélites (HJ-1C, Fengniao-1A y Xinyan-1). Fue enviado... órbita polar heliosincrónica. TIANWANG-1C 25.09.2015 China EXP... de altitud. También llamado TW-1C y NJFA-1. Es un minisatélite... Gran Bretaña COM STRV 1994- Gran Bretaña EXP STRV 1A 17.06...ña EXP STRV 1B 17.06.1994 Gran Bretaña EXP STRV 1C 16.11.2000 Gran Bretaña EXP STRV 1D 16... de 1 año. Satélite del programa STRV lanzado en la base de... los satélites INTELSAT 702 y STRV 1B. Pesaba 50 Kg y ten... Ecuador. Satélite del programa STRV lanzado en la base de... los satélites INTELSAT 702 y STRV 1A. Pesaba 53 Kg y ten... Kourou en compañía del INSAT 1C. Construido por la British Aerospace... India COM INSAT 1B INSAT 1C 30.08.1983 21.07....10.1994 India REC IRS-1C 28.12.1995 India REC... naturales, destinado a sustituir a los IRS-1C y IRS-1D. Dotado de paneles....04.2014 India NAV IRNSS-1C 15.10.2014 India NAV....07.1993 España COM HISPASAT 1C 03.02.2000 España COM....08.1994 Turquía COM TURKSAT 1C 09.07.1996 Turquía COM...). Viajó con los satélites STRV 1A y STRV 1B. Pesaba 3.695 Kg....1985 Liga Árabe COM ARABSAT 1C 26.02.1992 Liga Árabe...ñado del satélite TURKSAT 1C. Constrido por la Aerospatiale francesa....03.1991 ASTRA COM ASTRA 1C 12.05.1993 ASTRA COM... sustituir los antiguos ASTRA 1B y 1C de la serie. Vida útil... Ariane V56) junto al ASTRA 1C. Pesaba 154 Kg. Su órbita...



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0.15/5
GTO-HEO Orbites équatoriales à fortes excentricités Corps central Terre Type d’orbite GTO-HEO Usage Ceintures de Van Allen Missions spécifiques Nombre de satellites une dizaine Les trajectoires GTO (Geostationary Transfer Orbit) sont la voie d’accès aux orbites géostationnaires, avant les manœuvres d’apogée qui les placent sur leur trajectoire nominale. Les inclinaisons de ces trajectoires sont donc en général assez petites (inférieures à 10 degrés). On trouve sur ces orbites, en plus des satellites actifs (voir ci-dessous), de nombreux débris spatiaux issus des lancements, dont des derniers étages de fusée. La partie publique des catalogues de satellites recense une soixantaine d’objets dans ces régions. Les orbites GTO sont en général fortement excentriques, avec l’altitude du périgée de l’ordre de quelques centaines de kilomètres, et celle de l’apogée à environ 36 000 kilomètres. Elles ont des propriétés dynamiques très complexes, les perturbations au voisinage du périgée pouvant être dominées par le freinage atmosphérique et celles au voisinage de l’apogée par l’attraction luni-solaire. Ceintures de Van Allen Les ceintures de Van Allen ont été révélées par le premier satellite américain, Explorer-1, confirmé par Explorer-3, et dont le Principal Investigator a été James Alfred Van Allen (1914-2006). Ce sont des zones de radiation extrêmement nocives pour les organismes et l’électronique, situées entre, typiquement, 1 500 et 10 000 kilomètres d’altitude. Ces ceintures sont dues à des phénomènes d’interaction entre le milieu spatial et la magnétosphère terrestre. Les satellites de type GTO les traversent deux fois par révolution. Certains satellites ont pour mission la mesure de ces effets et en particulier : la mission américaine avec deux satellites RBSP (Radiation Belt Storm Probes ou Van Allen Probes), la mission anglaise de microsatellites STRV (pour Space Technology Research Vehicle). STRV-1B Orbite par rapport à la Terre Altit. équival. = 14233.5 km a =20611.604 km Inclinaison = 7.15 ° e = 0.679397 Phasage Période = 490.12 min * Révol./j.= 2.94 = [ 3;-12;161] 471 2010 05 26 06:29:17 TUC >>> 5.00 jours plus faible ; les points d’inflexion apparents (points de croisement) sont ceux où la vitesse du satellite correspond à la vitesse de rotation de la Terre (voir Figures 1 et 2). Les trajectoires se décalent un peu au cours du temps, car le nombre de révolutions par jour n’est pas exactement une fraction simple du jour sidéral (voir Table 1). STRV-1C Orbite par rapport à la Terre Altit. équival. = 19934.7 km a =26312.871 km Inclinaison = 6.02 ° e = 0.734470 Phasage Période = 707.12 min * Révol./j.= 2.04 = [ 2; +2; 69] 140 2010 02 15 08:33:45 TUC >>> 5.00 jours h_a = 39261 km ; h_p = 609 km ; arg. périgée : +226.14 ° h_a = 28237 km ; h_p = 230 km ; arg. périgée : +55.73 ° Projection : Orthographique Propriété : (sans) T.:Azimutal - Grille : 10° Centre Project.: 35.0 ° N ; 10.0 ° W Aspect : Oblique [ -90.0/ +55.0/+100.0] [-] EGM96 [NORAD] 2010 02 15 08:33:45 TUC / R: 6877 Noeud asc : -70.41 ° [03:52 TSM] Apogée : 88.21 ° F IGURE 2 – Représentation en repère terrestre sur 5 jours de l’orbite de STRV-1C Projection : Orthographique Propriété : (sans) T.:Azimutal - Grille : 10° Centre Project.: 35.0 ° N ; 10.0 °E Aspect : Oblique [ -90.0/ +55.0/ +80.0] [-] EGM96 [NORAD] 2010 05 26 06:29:17 TUC / R:15170 Noeud asc : -138.69 ° [21:15 TSM] Apogée : 155.21 ° F IGURE 1 – Représentation en repère terrestre sur 5 jours de l’orbite de STRV-1B Interprétation des figures La valeur de l’excentricité des GTO induit des variations de vitesse extrêmement importantes au cours d’une révolution. Ainsi que le prévoient les lois de Kepler, les points les plus proches de la Terre sont ceux où la vitesse est la plus grande, les points les plus éloignés ceux où la vitesse est la F. Deleflie, M. Capderou, (c) IMCCE - LMD - Ecole Polytechnique http://www.imcce.fr/fr/newsletter/archives.php TABLE 1 – Valeurs orbitales de satellites en orbite équatoriale excentrique. Les parenthèses correspondent à des satellites de la même famille d’engins (aux caractéristiques presque identiques) Apo./Pér. Exc. Incl. Période (km) (sd) (deg) (rev/j) STRV-1A (1B) 27 446/279 0.67 7.20 3.02 STRV-1C 39 261/609 0.73 6.02 2.04 RBSP-A (-B) 30 522/597 0.68 9.95 2.68 SPIRAL-A 17 533/347 0.56 2.00 4.56 SPIRAL-B 31 495/247 0.70 2.13 2.62 TEAMSAT 26 573/595 0.65 7.86 3.08 THEMIS-D (-E) 70 697/816 0.83 8.15 1.00 THEMIS-A 70 845/581 0.83 13.39 1.00 Taxinomie des satellites artificiels Juin 2015



Дата загрузки: 2017-04-24
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0.07/5
... GEO Feb 3 Atlas 2AS Hispasat 1C Feb 8 Delta 2 7420 Globalstars 60... 1R Success GEO AMSAT Phase 3-D STRV 1C STRV 1D Nov 21 Ariane 44L... radio payload, the LDREX and STRV technology experiments. Nevertheless, Ariane experienced... Energia ü Atlas 2AS CCAFS * Hispasat 1C Hispasat Zenit 2 Baikonur Kosmos 2369...- 6 ProSEDS * PAS 1R AMSAT Phase 3-D STRV 1C Kourou Plesetsk KSC 11/30... Development Agency RKK Energia Supply STRV 1D British MoD Progress MISS...



Дата загрузки: 2017-05-20
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0.17/5
...SSC97-X-6 STRV-lc & d Program Update Mr. Nigel ... Space Technology Research Vehicle (STRV-la and STRV-lb) spacecraft, the UK... and construction phase of the STRV-lc and -ld spacecraft commenced... report provides a program update on STRV-lc and -ld which presents... Introduction Full details of the STRV-la & b mission have been presented... Conference in . 12 prevIOus years ' . STRV ~ 1a & b, shown in an artist...'s ground stations in England. Fig 1 STRV~la In the light of the success of STRV-1 a & b, DERA has initiated STRV~lc & d as a follow... technologies flown as experiments on STRV-lc & d are associated with ongoing... automated ground station operations techniques. STRV~lc d will also exploit the... in the light of the STRV~la & b experience. This paper addresses the plans for the STRV~lc & d mission and describes the... AIAAIUSU Conference on Small Satellites • • • • • • • • • • • • • • • • • • • • • • • • • • • • • • • • • • • • • • • • • • • • • • • • • • • • • STRV-lc & d Mission I 2 3 14 5 6 7 8 9 10 II 12 Experiment Name STRV-Ie Amorphous Si solar cells... Cell Technologies Fig3 STRV-Ic&d I 13 14 The STRV-Ic & d mission is... the same design features as STRV-1 a & b however a number of modifications are... experiments compared to 15 on STRV-la & b. Together, these require significant... is therefore baselined for the STRV-lc & d mission. 15 16 18... 122 Sparc Microprocessor (# I ) Standard REM STRV-Id Coherent EM Radio tomography... IDERAIMitre MOD/ESAIDERAI MMS Table 1 STRV·Ie & d Payload Summary The experiments... in Table 2. I 2 3 4 5 6 7 8 9 Platform Technology Name STRV-lc GaAs/Ge solar panels.../Ge & GaAs/GaAs solar panels STRV-ld InP solar panel GaAs... DoD(BMDO)/PL BNSCIDERAI AEAT STRV-lc & d Demonstration Platform Technologies • Demonstrating... of enhancements to the basic STRV-1a/b platform are being made... of the instrument flown on STRV-1 b), which provides electron and proton... developed from that flown on STRV-1a and the APEX mission.... Both devices under-performed on STRV-la & b and although this did... solar aspect angle experienced on STRV-1a & b. • Mapping equatorial ionospheric electron... subsystem architecture for STRV-lc & d is unchanged from the STRV-1a & b design... key features of STRV1a/b and STRV-1c/d is given in Tables 3a... ± 3°. Magnetorquer & cold gas thruster manoeuvres (STRV-la only). Sun & Earth aspect... ground operations of STRV -1 c & d. Ground station linking with STRV -1 a & b was conducted under... angle"" 90° ± 10° Table 3a STRV-Ia & b CharacterIStIcs (per vehicle) Total... a switched Li-ion battery on STRV-\d i Regulated 28V ± 2% Mil. spec. 317... & TC (with optional encryption on STRV-ld) S band at lkbps S band...° & orbit normal ± 10°. Table 3b STRV-lc & d CharacterIStics (per vehicle) 6 Mr... Satellites • • • • • • • • • • • • • • • • • • • • • • • • • • • • • • • • • • • • • • • • • • • • • • • • • • • • • SCPS software experiment to STRV-I b during the second year of... UK. The architecture of the STRV-Ic & d ground segment is shown... who participated in STRV -I a & b are flying experiments on STRV -1 c & d and that a number... program. NdwQrklnterface - .:::~:: STRV 1 c&d Ground Segment ." OERA lasham Fig 4 STRV-lc & d Ground Segment... a space technology research vehicle with STRV -1 a & b, it is possible to focus... design to operations, achieved with STRV-la & b, is being reduced to 2 years for STRV lc & d. Although there have been... sophistication. Current Program Status The STRV-lc & d program completed Project Definition.... However, the lessons learned form STRV 1a&b indicate that there may... the decade. Conclusions Acknowledgements The STRV-la &. b mission has proved much... gratefully received contributions of the STRV-la & b and -Ic & d project teams... SSTL Surrey Satellites Technology Ltd, STRV Space Technology research Vehicle TC... Southampton Mr. Wells is the STRV-laJb Mission Manager in the... and Deputy Project Manager for STRV-lc & d. and has been a member... BSc MIEE CEng is the STRV -1 c & d Project Manager. He joined the... Engineer. References 1. Wells et aI, "STRV-laJb : The first Results", Proc..., "The Space Technology Research Vehicles STRV-Ia,b,c & d", Proc. 10th Ann. AIAAIUSU...



Дата загрузки: 2017-01-16
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0.05/5
... the same time as FY-1C, is in a circular Sun-synchronous...-30) on 3 September 1990, FY-1C (DFH-46) on 10 May... 30 August 1983 (STS8), INSAT-1C on 21 July 1988, INSAT... on 29 August 1991, IRS-1C on 28 December 1995, IRS... 20 September 1993 (before IRS-1C), failed, IRS-P2 on 15... in 2000, followed by Beidou-1C (DFH-56) in 2003. (‘Beidou...◦ E, Gorizont31 (Russia) 39.91◦ E, Turksat-1C (Turkey) 41.99◦ E, Intelsat-704..., we find the British microsatellites STRV (Space Technology Research Vehicle), hp... km, ha = 36 000 km, i = 7◦ , STRV-1A and -1B launched in... passengers with Intelsat-702, and STRV-1C and -1D in 2000, passengers...



Дата загрузки: 2016-12-24
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...) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . D.17.4 IRS-P2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . D.17.5 IRS-1C/1D . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . D.17.6 IRS-P3 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . D.17...) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . G.3.1 FY-1A, -1B . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . G.3.2 Feng-Yun-1C and -1D . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . G.3.3 Feng-Yun-3 (FY... STRV (Space Technology Research Vehicle) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . M.25.1 STRV-1a and -1b . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . M.25.1.1 STRV-1a Sensor/Experiment Complement . . . . . . . . . . . . . . . . . . M.25.1.2 STRV-1b Sensor/Experiment Complement . . . . . . . . . . . . . . . . . . M.25.2 STRV-1c and -1d . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . M.25.2.1 STRV-1c Sensor/Experiment Complement . . . . . . . . . . . . . . . . . . M.25.2.2 STRV-1d Sensor...-5 (Tri-Service Experiments Mission 5) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . M.29.1 STRV-2 (Space Technology Research Vehicle-2) . . . . . . . . . . . . . . . . . . . . . . M.29...