Спутник технологический. QubeScout-S1. [Редактировать]

QubeScout-S1 масой 1 кг, разработан студентами университетов Германии и предназначен для отработки перспективных технологий

Дополнительная классификация

#Наименования
1Страна производитель - Германия
2Страна оператор(владелец) - Германия

Технические характеристики

#ХарактеристикаЗначение
1Масса, кг0.4

Информация об удачном запуске

#ХарактеристикаЗначение
1Космодром Пусковая база Ясный
2Дата пуска2013-11-21 at 07:10:00 UTC
3Полезная нагрузка 1xAprizesat 7
4Полезная нагрузка 1xSkySat 1
5Полезная нагрузка 1xSTSAT 3
6Полезная нагрузка 1xDubaiSat 2
7Полезная нагрузка 1xWNISAT-1
8Полезная нагрузка 1xBRITE-PL
9Полезная нагрузка 1xAprizesat 8
10Полезная нагрузка 1xUniSat-5
11Полезная нагрузка 1xDelfi-n3Xr
12Полезная нагрузка 1xDove-3
13Полезная нагрузка 1xDove-4
14Полезная нагрузка 1xTriton-1
15Полезная нагрузка 1xCINEMA 1
16Полезная нагрузка 1xCINEMA 2
17Полезная нагрузка 1xOPTOS
18Полезная нагрузка 1xCubeBug-2
19Полезная нагрузка 1xGOMX-1
20Полезная нагрузка 1xNEE-02
21Полезная нагрузка 1xFUNcube-1
22Полезная нагрузка 1xHiNCube
23Полезная нагрузка 1xZACUBE-1
24Полезная нагрузка 1xICube-1
25Полезная нагрузка 1xHumSat-D
26Полезная нагрузка 1xPUCP-SAT-1
27Полезная нагрузка 1xFirst-MOVE
28Полезная нагрузка 1xUWE-3
29Полезная нагрузка 1xVELOX-P-2
30Полезная нагрузка 1xBeakerSat-1
31Полезная нагрузка 1x$50SAT
32Полезная нагрузка 1xQubeScout-S1
33Полезная нагрузка 1xWren
34Полезная нагрузка 1xPocket-PUCP
35Ракета-носитель 1xДнепр

Найдено 12 документов по запросу «QubeScout-S1». [Перейти к поиску]


Дата загрузки: 2017-01-30
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0.08/5
... для отработки перспективных технологий. КА QubeScout-S1 разработан и изготовлен в американском Мэрилендском университете...-P2, Сингапур, 1 кг $50sat, США QubeScout S1, США, 0,4 кг Wren, Германия, 0,250...



Дата загрузки: 2016-11-15
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0.14/5
.... The NanoSat is called Qubscout-S1 and measures 2 in x 2 in x 5 in... Mrs. Barbara Schoeberl). satellite mission. Qubescout-S1 was launched from Yasny, Russia... change its rotation rate. Qubscout-S1 was built as a joint venture between STC and UMBC. Qubscout-S1 will test a UMBC designed micro... educational program of which the Qubescout initiative was part of. Other... our costs very low." Qubscout-S1 was built in 2010, but... was launched this year. Qubscout-S1 was orbited – Continued on page...



Дата загрузки: 2017-11-08
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0.18/5
COLLISION AVOIDANCE STRATEGIES, IMPLEMENTATION AND OPERATIONAL EXPERIENCE FOR DEIMOS-1 AND DEIMOS-2 MISSIONS Mar Luengo Cerrón(1), Carlos Díaz Urgoiti(2), Fernando Gonzalez Meruelo(3), Annalisa Mazzoleni(4), Patricia Pisabarro Marrón(5), Fabrizio Pirondini(6) (1) Deimos Imaging, Parque Tecnológico de Boecillo, Edificio Galileo, Módulo Gris, Oficina 103, Boecillo (Valladolid), Spain, +34 983548923, mar.luengo@deimosimaging.com (2) Deimos Imaging, carlos.diaz@deimos-imaging.com (3) Deimos Imaging, fernando.gonzalez@deimos-imaging.com (4) Deimos Imaging, annalisa.mazzoleni@deimos-imaging.com (5) Deimos Imaging, patricia.pisabarro@deimos-imaging.com (6) Deimos Imaging, fabrizio.pirondini@deimos-imaging.com Abstract: Deimos Imaging (Spain), a subsidiary of UrtheCast Corp. (Canada), owns two commercial Earth Observation (EO) missions, DEIMOS-1 and DEIMOS-2. Deimos Imaging is in charge of operating both satellites and commercialising their imagery. Launched in 2009, DEIMOS-1 is a 100-kg satellite based on SSTL-100 platform equipped with a warm-gas resistojet, and currently at the beginning of its 5-year extended lifetime. Launched in mid-2014, DEIMOS-2 is a 300-kg satellite based on Satrec Initiative SpaceEye-1 platform equipped with a low-thrust Hall-Effect plasma thruster. Both missions fly on Sun-Synchronous Low Earth Orbit (LEO), with mean altitudes of 660 km for DEIMOS-1 and 620 km for DEIMOS-2. This orbit environment is known for its high density of operational and non-operational objects, and thus an efficient Collision Avoidance (CA) procedure is of key importance to assure the survivability of each mission. This paper presents an overview of Deimos Imaging Collision Avoidance activities, based on the operational experience for DEIMOS-1 and DEIMOS-2 missions. Operational tools, theories and procedures used are outlined, aided by real-life examples of conjunction events. Keywords: DEIMOS-1, DEIMOS-2, Collision Avoidance 1. Introduction DEIMOS-1 and DEIMOS-2 missions are fully owned and operated by Deimos Imaging (Spain), a subsidiary of UrtheCast Corp. (Canada). Successfully launched in July 2009, the DEIMOS-1 satellite is currently at the beginning of its 5-year extended lifetime, while the DEIMOS-2 satellite, launched in June 2014, is at the beginning of its 10 years of expected lifetime. DEIMOS-1 is equipped with a multi-spectral optical instrument, having a spatial resolution of 22 m and a very wide swath of 650 km. Its imagery is mainly used for large-scale agriculture applications worldwide. DEIMOS-2 is an agile 300-kg satellite for very-high-resolution Earth Observation applications. It provides 75-cm pan sharpened images with a swath of 12 km at nadir, mainly for mapping, monitoring and security applications. Both satellites are equipped with a propulsion system providing thrust in the millinewton range, with a specific impulse around 100 s for DEIMOS-1 (warm-gas resistojet), and 1000 s for DEIMOS-2 (Hall Effect Thruster). They both underwent a large orbit manoeuvring campaign just after launch, aimed at reaching the nominal operational altitude and ensuring an optimal natural (uncontrolled) evolution of the Local Time at Ascending Node (LTAN). After these initial campaigns had been successfully carried out, the activities of the Flight Dynamics (FD) team are centred on collision avoidance issues. Both missions fly on Sun-Synchronous LEO, with mean altitudes of 660 km for DEIMOS-1 and 620 km for DEIMOS-2. This orbit environment is quite littered with space debris, and an efficient Collision Avoidance (CA) procedure is of key importance for assuring the survivability of each mission. In order to maximise the effectiveness of the CA, Deimos Imaging FD team is in constant communication with the Joint Space Operations Center (JSpOC). The need to give a quick and sensible answer to Conjunction Data Messages (CDMs) received from JSpOC drove the creation of the internal tools and operational procedures which are now the backbone of Deimos Imaging CA strategy. A first set of tools, aimed at anticipating possible close approaches by using multiple TLEs to refine the orbit of an object, provide quick results and help the operators to easily assess the characteristics of any possible close approach. Additionally, tools to compute the collision probability and geometry at the B-plane based on CDM data are also available and used in actual operations to ease the decision-making process. Besides, tools implementing the latest developments in algorithms to create avoidance strategies are used to cross-check and refine the avoidance strategy. Finally, visualization and data-distribution tools are continuously being improved to guarantee that relevant information is made available to the appropriate people in a clear and concise manner. This paper presents an overview of Deimos Imaging Collision Avoidance activities, based on the operational experience for DEIMOS-1 and DEIMOS-2 missions. Operational tools, theories...



Дата загрузки: 2017-04-09
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0.03/5
...-P-2 (Сингапур) BeakerSat-1 (США) $50SAT (США) QubeScout-S1 (США) Wren (Германия) Pocker-PUCP...



Дата загрузки: 2017-05-20
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0.03/5
...-MOVE, Manolito, Krysaor, PUCP-Sat-1, QubeScout-S1, FUNcube-1, HiNCube-1, UWE-3 [10] 3118...



Дата загрузки: 2017-06-15
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0.21/5
... volume. TLogoQube, WREN, Eagle-1, and QubeScout-S1 are all PocketQube satellites that...



Дата загрузки: 2017-09-24
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0.18/5
... volume. TLogoQube, WREN, Eagle-1, and QubeScout-S1 are all PocketQube spacecraft examples...



Дата загрузки: 2016-11-04
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0.03/5
...-1 39442 145.840 1200bps AFSK i Qubescout-S1 39443 . 9600bps GMSK i FUNcube-1 (AO... 0 9k6 1 U 436.006 435.982 S1 2400.768 2400.740 S2... 2-Uplink, L1 & L2 2-Uplink, 2-Downlink, S1 & S2 Uplink Downlink Downlink Beacon....830 460.540 581.500 | | | | S1 2421.580 2425.290 2546....050 24483.825 | |_ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _| | | | L1 L2 S1 S2 C | | V 1415.275 1414.350....075 2882.175 6104.275 | | | | S1 3669.725 3668.800 8069....495 1269.360 - 1269.211 S1-Dw S2-Dw : : 2400.245...



Дата загрузки: 2017-02-06
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0.13/5
....11.24 2013.11.24 QubeScout S1 Wren US DE 185 2013...



Дата загрузки: 2017-02-23
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0.18/5
... volume. TLogoQube, WREN, Eagle-1, and QubeScout-S1 are all PocketQube satellites that...