Спутник технологический. STRV 1D. [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 1D

Технические характеристики

#ХарактеристикаЗначение
1Масса, кг101.5
2Габариты, метра0.7х0.7х0.7
3Мощность, Вт80

Пусковые характеристики

#ХарактеристикаЗначение
1Код NSSDC2000-072D

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 15 документов по запросу «STRV 1D». [Перейти к поиску]


Дата загрузки: 2016-11-02
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....02.1967 Francia GEO DIADEME 2 D-1D 15.02.1967 Francia GEO....06.2000 China MET FY-1D 15.05.2002 China MET....05.2003 China NAV BEIDOU 1D 02.02.2007 China NAV... también llevó al Feng Yun 1D. Fue enviado a una órbita polar... Gran Bretaña COM STRV 1994- Gran Bretaña EXP STRV 1A 17.06.1994 Gran Bretaña EXP STRV 1B 17.06.1994 Gran...ña EXP STRV 1C 16.11.2000 Gran Bretaña EXP STRV 1D 16.11... 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... India India COM COM INSAT 1D 12.06.1990 India COM....03.1996 India REC IRS-1D 29.09.1997 India REC... a sustituir a los IRS-1C y IRS-1D. Dotado de paneles solares, pesaba....10.2014 India NAV IRNSS-1D 28.03.2015 India NAV... un cuarto satélite, el 1D, para satelizar en principio en... Ku –de 36 MHz y HISPASAT 1D 18.09.2002 España AMAZONAS...). Viajó con los satélites STRV 1A y STRV 1B. Pesaba 3.695 Kg....05.1993 ASTRA COM ASTRA 1D 01.11.1994 ASTRA COM...



Дата загрузки: 2016-12-24
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....4 IRS-P2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . D.17.5 IRS-1C/1D . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . D.17.6 IRS-P3 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . D.17.7 IRS..., -1B . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . G.3.2 Feng-Yun-1C and -1D . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . G.3.3 Feng-Yun-3 (FY-3) Satellites . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . METEOR... 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...



Дата загрузки: 2016-10-31
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... COSMOS 0141 COSMOS 0142 DIADEME 2 D-1D KH 4A-1039 KH 8-04... KRISTALL ROSAT NOSS 09 INSAT 1D MOLNIYA 3-38 COSMOS 2083 GORIZONT... 2281 FOTON 9 INTELSAT 702 STRV 1A STRV 1B UHF F03 STEP-1/P90...-7 EKSPRESS 1 IRS-P2 ELEKTRO ASTRA 1D WIND COSMOS 2293 RESURS O1... IRIDIUM 36 IRIDIUM 37 IRS-1D ECHOSTAR 3 PROGRESS M-36 FOTON 11... 49 OSCAR 40 PANAMSAT 1R STRV 1C STRV 1D PROGRESS M1-4 QUICKBIRD 1 ANIK... IDÉFIX SPOT 5 DIRECTV 5 FY-1D HAIYANG-1 OFFEQ-5 COSMOS 2389 INTELSAT... DRTS-W USERS METSAT HTSTL-1 HISPASAT 1D PROGRESS M1-09 NADEZHDA 7 FOTON... 1 SRE 1 PROGRESS M-59 NSS-8 BEIDUOU 1D THEMIS IGS 3B STP-1 STPSAT... otras aplicaciones 108 FLOCK 1D-01 a FLOCK 1D-26 GOMX-2 RACE GPS... FY-2G AESP-14 FLOCK 1D-1 FLOCK 1D-2 CRS-5 MUOS-3 SMAP GRIFEX...-9 IGS OPTICAL 5 GALILEO 7 GALILEO 8 IRNSS-1D 28.10.2014 USA De...



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...-II, EXEQ I to IV, MPTB, STRV, EVALCOMP, ICARE, COMRAD, SPICA, SPICA... Carrier SPOT-4 SPOT-4 MIR MPTB STRV 1d MIR SAC-C ISS STENTOR Orbit...). Due to the failure of STRV 1c/d in its early days... ETB (Electronics Test Bed) on STRV 1c/d. The principle of the...



Дата загрузки: 2017-02-06
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... Technology Research Vehicle microsatellites, STRV 1C and STRV 1D. Gülzow says Phase 3D...



Дата загрузки: 2016-12-24
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... following: Space Technology Research Vehicle (STRV) -1d, Korea Multipurpose Satellite-II (KOMPSAT... Spacecraft, Canadian satellite RADSAT-2 [4, 5, 6, 7]. The STRV, MetOp and RADSAT employ the...



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... 6.2 2000-072C STRV 1C UK 680 39790 6.3 2000-072D STRV 1D UK 602...



Дата загрузки: 2017-02-23
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... Technology Research Vehicles . . . . . . . . . . . . . . . 98 5.1.4 Future STRV Missions . . . . . . . . . . . . . . . . . . . . . . 100 New Reflector... Shuttle Radar Topography Mission, p. 16 STRV Space Technology Research Vehicle, p. 96... 2π v 2πi v , (3.1b) R sin θ + −R sin R sin H , (3.1c) T 2π v 2π v T 2πi v , 0 (3.1d) T 0 . (3.1e) The kinematic form-finding... AND DEPLOYABLE STRUCTURES STRV ASAP Figure 5.1: DERA’s small satellites STRV-1 C and D on... the Space Technology Research Vehicle (STRV) programme as a single micro-satellite... micro-satellites of the programme, STRV-1 A and B, were launched on June...) [32]. The dimensions of both STRV-1 A and B were 0.45 × 0.45 × 0.47... W [32]. Unlike the Astrid satellites, STRV-1 A and B had no deployable structures... panels. The design lifetime of STRV-1 A and B was one year, but... [32]. Following the success of STRV-1 A and B, DERA designed two new... power available on STRV-1 A and B. The dimensions of STRV-1 C and D were 0.7 × 0.6 × 0.7 m3... satellite weighed about 100 kg. STRV-1 C and D were launched on November... FOR A DEPLOYABLE REFLECTOR ANTENNA 5.1.4 Future STRV Missions In the spring of... started the plans for future STRV missions. The main areas of... by the envelope around the STRV-1 C and D satellites on the Ariane... view Figure 5.4: Envelope of the STRV on ASAP ring (Courtesy of... the stowage requirements of a future STRV mission. Ideally, the required accuracy... developing deployable structures for the STRV. As mentioned earlier, a parabolic antenna... full scale antenna for a future STRV mission will be designed. First... antenna is suitable for a future STRV mission, some issues remain that... Agency. Space Technology Research Vehicle (STRV). http://www.dera.gov.uk/html/space/strv/home.htm (21 June 2001...



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...) on 10 May 1999, FY-1D (DFH-53) on 15 May... Satellites by Mission Feng Yun-1D Orbit - Ground track Altitude = 859... on 21 July 1988, INSAT-1D on 12 June 1990, INSAT... on 28 December 1995, IRS-1D on 4 June 1997, IRS-1E... 12 May 2002 (with FY-1D). In preparation: HY-2 (Ocean-2). 214..., we find the British microsatellites STRV (Space Technology Research Vehicle), hp... km, ha = 36 000 km, i = 7◦ , STRV-1A and -1B launched in... with Intelsat-702, and STRV-1C and -1D in 2000, passengers with...



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Archive November 17, 2000 STRV-1c/d Successful Launch The Ballistic Missile Defense Organization (BMDO) announced today that the Space Technology Research Vehicles-1c and -1d (STRV-1c/d) microsatellites were successfully launched into Geo-Transfer Orbits (GTO) at 8:07pm, Wednesday, November 15, 2000. The two microsatellites were assembled by the UK Ministry of Defence, Defence Evaluation and Research Agency (DERA) and launched on an Arianespace Ariane-V rocket from Kourou, French Guiana. The STRV1c/d satellites were secondary payloads with PanAmSat the primary payload. Preliminary data from the spacecraft indicate that STRV-1c/d satellites are in the planned orbit and fully operational. The two satellites host a total of 25 hardware and three software experiments provided by multiple sponsors including the BMDO, the United Kingdom Ministry of Defence, the United States Air Force, the United States Navy, the DoD Space Test Program (STP), the National Aeronautics and Space Administration (NASA) and the European Space Agency (ESA). The BMDO experiments include an advanced quantum-well infrared photometer (QWIP) experiment, an experimental multifunctional structure (MFS), and an Electronics Testbed (ETB). The STP sponsored experiments include the Air Force Research Laboratory (AFRL) Compact Environmental Anomaly Sensor (CEASE) and the Naval Research Laboratory (NRL) Coherent Electromagnetic Radio Tomography/Profiling the Limb with UV Sensors (CERTO/PLUS). The QWIP experiment will quantify the effects of on-orbit radiation on the performance of this advanced sensor concept. The MFS experiment will demonstrate the integration of thermal control, cables and harnesses, power distribution and storage, and electronics into the load-bearing spacecraft structure. The ETB will obtain data on performance of advanced micro-electronics for DoD and civilian systems in a high radiation environment. CEASE will demonstrate the ability of a small spacecraft-mounted sensor package to warn operators during conditions of potential surface charging, deep dielectric charging and single-event upsets. CERTO PLUS will provide measurements of the integrated electron density of the ionosphere. CERTO/PLUS will also test and validate tomographic algorithms for reconstruction of ionospheric densities and irregularity structures.