Спутник ДЗЗ. STPSat-3. [Редактировать]

КА STPSat-3 создан специалистами компании Ball Aerospace по заказу Центра космических и ракетных систем ВВС США, он предназначен для проведения экспериментов в интересах американских военных и NASA.

Дополнительная классификация

#Наименования
1Страна оператор(владелец) - США
2Страна производитель - США
3Все спутники ДЗЗ

Информация об удачном запуске

#ХарактеристикаЗначение
1Космодром Уоллопс
2Дата пуска2013-11-20
3Полезная нагрузка 1xKySat-2
4Полезная нагрузка 1xSTPSat-3
5Полезная нагрузка 1xPrometheus 1A
6Полезная нагрузка 1xPrometheus 1B
7Полезная нагрузка 1xPrometheus 2A
8Полезная нагрузка 1xPrometheus 2B
9Полезная нагрузка 1xPrometheus 3A
10Полезная нагрузка 1xPrometheus 3B
11Полезная нагрузка 1xPrometheus 4A
12Полезная нагрузка 1xPrometheus 4B
13Полезная нагрузка 1xHorus
14Полезная нагрузка 1xORSES
15Полезная нагрузка 1xORS Tech 1
16Полезная нагрузка 1xORS Tech 2
17Полезная нагрузка 1xSENSE 1
18Полезная нагрузка 1xSENSE 2
19Полезная нагрузка 1xH2 sat
20Полезная нагрузка 1xDragonSat-1
21Полезная нагрузка 1xNPS-SCAT
22Полезная нагрузка 1xFirefly
23Полезная нагрузка 1xSPA-1
24Полезная нагрузка 1xChargerSat
25Полезная нагрузка 1xLunar
26Полезная нагрузка 1xCOPPER
27Полезная нагрузка 1xBlack Knight-1
28Полезная нагрузка 1xSwampSat
29Полезная нагрузка 1xCAPE-2
30Полезная нагрузка 1xTJ3Sat
31Полезная нагрузка 1xPhoneSat 2.0
32Ракета-носитель 1xМинотавр 1

Найдено 66 документов по запросу «STPSat-3». [Перейти к поиску]


Дата загрузки: 2016-12-09
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0.12/5
... launch alternative. STP Satellite Mission 1 (STPSat-1) is the first STP satellite... specifically to exploit this capacity. STPSat-1 continues STP’s mission to provide... their weighting. In these respects, STPSat-1 is typical of all engineering... generally, two requirements drive the STPSat-1 design: 1) satisfy the requirements of... constraints have affected the ultimate STPSat-1 design. STPSat-1 Mission Overview Space Test... mission planning and Figure 1. The STPSat-1 Spacecraft Design is Driven by... STPSat-1 throughout the mission lifetime. Table 1 summarizes the organizational elements of STPSat... are very limited, STP Table 1. STPSat-1 Organizations and Their Roles and.../ST) Overall Mission Management for STPSat-1 and Mission Management for the... AeroAstro, Inc. Prime contractor for STPSat-1 spacecraft bus, experiment integration, system...; support experiment mission operations through STPSat-1 mission life • Naval Research Lab... (IPTs) to manage the STPSat-1 program. The STPSat-1 team holds weekly Operations... STPSat-1 program envisions a three-year development schedule (including several Figure 2. The STPSat...-05 launch schedule risk. The STPSat-1 experiments have varying degrees of... conducted. At this writing, the STPSat-1 program anticipates SV Critical Design... in November 2002. Payload Instrumentation STPSat-1 hosts four experiments selected by... Equipment (GFE) to AeroAstro. The STPSat-1 Principal Investigators (PIs) who are.... SHIMMER, the primary payload on STPSat-1, is a high-resolution ultraviolet spectrometer... design drivers for STPSat-1. WSSP , a secondary payload on STPSat-1, is a 6U Versa... Figure 5), another secondary payload on STPSat-1, is a tri-frequency receiver Figure... a multi-band antenna located on STPSat-1. Beacons from the Coherent Electromagnetic... situational awareness. MEPSI, the third STPSat-1 secondary payload, contains a pair of... from STPSat-1. The PicoSats can then be operated independently of STPSat-1 for... Transform Spectrometer (IOMI/GIFTS). Besides STPSat-1, the other secondary SVs include... MLV-05 Payload Complement (Note: STPSat-1 is shown in a conceptual configuration... into a Geostationary Transfer Orbit. However, STPSat-1 also fills a unique role as... fully understood how STPSat-1 as an ESPA Pathfinder STPSat-1 is the next... yet another constraint: on the STPSat-1 project cost. The ESPA demonstration... demands STP’s funding and attention. STPSat-1 is funded using residuals from..., STPSat-1 is a design-to-cost mission. The funding available for the STPSat... documentation. By planning and executing STPSat-1, STP will gain first-hand... take advantage of ESPA opportunities. STPSat-1 Space Vehicle Overview The PDR... the Payload Module. Figure 9. The STPSat-1 Vehicle Davis, Patricia 9 16th Annual... subsequent sections. STPSat-1 Design Challenges Designing to Payload Requirements The STPSat-1 spacecraft... design. The four payloads on STPSat-1 perform significantly different types of... power-hungry star tracker. The STPSat-1 spacecraft has a high power density... 9 months after award of the STPSat-1 contract, and 2 months after Preliminary... to completely envelope potential environments. STPSat-1 is being designed with a minimum... current design loads envelope for STPSat-1. A "mini coupled loads analysis" has... the same orbit as STPSat-1), this requires STPSat-1 to be capable of... the LV Integrating Contractor. Since STPSat-1 will be unpowered throughout ascent... research and development (R&D) satellites, therefore, STPSat-1 can expect to get about... existing ground network (the AFSCN), STPSat-1 is also designed to interface... (three TechSat-21 vehicles and STPSat-1), STPSat-1 is designed to be operationally... Other "operator friendly" features of STPSat-1 include: autonomous entry into safe... New Technologies As highlighted previously, STPSat-1 is highly constrained by a number... and selected special testing. Since STPSat-1 utilizes GPS for both timing... launch and on-orbit environments. STPSat-1 seeks to use heritage components... StarSys Research. Designing to Cost STPSat-1 is a very cost-constrained program... regard to providing payload support, STPSat-1 is essentially a design-to-cost... test time and costs. While STPSat-1 uses no explicitly redundant subsystems... without flying a fully redundant battery. STPSat-1 is also implementing a policy of..., however. STPSat-1 has selected to take a middle ground: wherever possible, STPSat-1 will... the best tradeoff and help STPSat-1 minimize costs while maximizing reliability... also preserves flexibility to adapt STPSat-1 quickly and easily for different... Program and the STPSat-1 Space Vehicle (including the STPSat-1 experimental payloads), concluding... that will carry STPSat-1 into orbit. We then discussed STPSat-1's unique role... role causes significant difficulties for STPSat-1 given the dearth of flight... parameters that have shaped the STPSat-1 design, including Payload requirements, LV... paper focused on how the STPSat-1 design incorporates new technologies when... spacecraft design has emerged for STPSat-1 that satisfies these many conflicting...



Дата загрузки: 2016-12-09
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0.11/5
SSC07-VII-5 STPSat-1: The First Space Test Program ... The Space Test Program Satellite-1 (STPSat-1) mission is the first STP... Adapter (ESPA). At this writing, STPSat-1 is fully operational on-orbit... vehicle (AV-013 / STP-1). The STPSat-1 space vehicle hosts two DoD... technical challenges encountered by the STPSat-1 team during the development cycle... on a DoD EELV launch. Because STPSat-1 is launched on the first... the new ESPA launch capability. STPSat-1’s primary experiment, built by the... in the middle INTRODUCTION AeroAstro’s STPSat-1 is the first commercially developed... ESPA developed by the USAF. STPSat-1 was successfully launched on March... 1). The primary mission objectives of STPSat-1 are: to provide a successful one... and commanding services to the STPSat-1 mission. The Space Test Group... required services. SPACECRAFT OVERVIEW The STPSat-1 space vehicle (see Figure 2) consists... the top face of the STPSat-1 satellite. Transmissions from Coherent Electromagnetic... solar arrays deployed. A picture of STPSat-1 in its stowed configuration is... on Small Satellites ESPA INTERFACE STPSat-1 is mechanically attached to the.... The Lightband attaches to both STPSat-1 and the ESPA with 24... two halves of the device. STPSat-1 EDU Lightband Photograph reprinted courtesy... States Air Force. ESPA Figure 2: STPSat-1 Space Vehicle Prior to Launch... 4: Lightband Separation System mounted to STPSat-1 EDU and ESPA Use of... access to the Lightband when STPSat-1 was mounted to the ESPA.... Limited access between the integrated STPSat-1/Lightband and the ESPA ring... mitigate this, AeroAstro sent the STPSat-1 Engineering Development Unit (EDU) structure... United States Air Force. Figure 3: STPSat-1 in Stowed Configuration (mounted to... Conference on Small Satellites NextSat). STPSat-1 on the IPS is shown... plane change and then released STPSat-1 at a target circular orbit of... Another challenge faced by the STPSat-1 design team was that the... with the launch vehicle’s transponder. STPSat-1 was one of five spacecraft...) included the four ESPA spacecraft (STPSat-1, MidStar-1, FalconSat-3, Cibola Flight Experiment... to the long period that STPSat-1 remained on the IPS before... presented a potential thermal issue for STPSat-1. Fortunately, the IPS maintained a “rotisserie... IPS roll kept STPSat-1 within its thermal specifications. Other STPSat-1 time constraints... damping was cut short. Also, STPSat-1 required deployment either in the... time constraint consideration for the STPSat-1 deployment included delta-velocity separation... site operations. For this document, STPSat-1 was required to provide a list... from the Atlas/Centaur before STPSat-1. OE deployment presented a shock event... after STPSat-1 had begun integration. The risk here was that some STPSat..., etc), their location on the STPSat-1 spacecraft, and review heritage shock... vehicle and other integrated satellites. STPSat-1 has multiple levels of ‘inhibits... the design of FPGAs). The STPSat-1 design also included monitor points... concern to range safety was STPSat-1’s use of Lithium-ion (Li..., was in close proximity to STPSat-1 and radiated at a power sufficient...’s transmitter. LAUNCH RANGE SAFETY CONSIDERATIONS STPSat-1 was launched from Cape Canaveral.../USU Conference on Small Satellites STPSat-1’s approaches to these issues are... testing of cell venting. The STPSat-1 electrical power system (shunt regulator... charging was stopped. To ensure STPSat-1’s optimal configuration of arriving on... scrutiny. Initial battery charging on STPSat-1 while mated to the launch... performed safely. Periods of charging STPSat-1 batteries on the launch vehicle... at the launch site on STPSat-1 resulted in an optimum battery... for the SHIMMER instrument on STPSat-1, Applied Optics, 42, 2829-2834..., 80, 473-485, 2006. CONCLUSION STPSat-1 was successfully launched on March... site related issues faced by STPSat-1 are likely to be faced...



Дата загрузки: 2016-12-29
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0.1/5
... flying in low earth orbit . STPSat-1, a spacecraft developed by STP for... five secondary spacecraft (three TechSats, STPSat-1, and NPSat1) will be deployed... make the testing more difficult. STPSat-1 (similar in mass to the... ? Vs for the TechSats and STPSat-1 are no more than 0.4 m/sec...° apart around the ESPA ring. 2) STPSat-1 and NPSat-1 have no on... over the course of a year. STPSat-1’s orbit average ballistic coefficient with... kg/m2 . The arrays on STPSat-1 do not change orientation with... natural possibilities are: 1) NPSat-1 and STPSat-1 get positive ?Vs and the... it will fall behind, and STPSat-1 will be in between as... quickly and TS1 a TS2 a TS3 a STPSat a NPSat a a= along track acceleration relative... 2: Natural Order b) Since NPSat-1 and STPSat-1 are each opposite a TechSat on... two whose STPSat TS3 Rotate 120° Upper Stage velocity TS3 ?v STPSat ESPA... (m/sec) ?V Direction (+ or – velocity) NPSat-1 0.4 + STPSat-1 0.3 + TechSat #1 0.4 TechSat #2 0.3 TechSat #3 0.2 Table 1: ?V Sizes... m/sec for the TechSats and STPSat and 0.02 to 0.04 m/sec... direction. Five minutes later, Deploy STPSat-1 with a ?V of approximately 0.3 m/sec in..., but then the ?Vs for STPSat-1 and the TechSats would need...



Дата загрузки: 2016-12-20
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0.08/5
... for the SHIMMER instrument on STPSat-1 John M. Harlander, Fred L. Roesler, Christoph... Earth orbit aboard the satellite STPSat-1 scheduled for launch in 2006... for launch on STPSat-1 in March 2006. SHIMMER STPSat-1 is the second... for the SHIMMER instrument on STPSat-1 5b. GRANT NUMBER 5c. PROGRAM... that will be imaged on STPSat-1. The dispersion plane of the... the interferometer integrated in its STPSat-1 flight fixture. We also performed... the expected temperature range of STPSat-1 on an optically contacted part... for launch on STPSat-1 in March 2006. SHIMMER STPSat-1 will view the...͒. The SHIMMER Middeck and SHIMMER STPSat-1 missions are a joint effort between...



Дата загрузки: 2016-12-29
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SCC07-VII-5 STPSat-1: The First Space Test Program ... technical challenges encountered by the STPSat-1 team during the Space Vehicle... Air Force. SSC07-VII-5 - Page 2 STPSat-1 Background ¾ First AF-developed spacecraft...-1 ¾ The primary mission objectives of STPSat-1 are: – To provide a successful oneyear... Air Force. SSC07-VII-5 - Page 3 STPSat-1 Experiments ¾ ¾ ¾ Primary experiment is the... the top face of the STPSat-1 satellite – Transmissions from ground French... Air Force. SSC07-VII-5 - Page 4 STPSat-1 Space Vehicle ¾ SV consists of.... SSC07-VII-5 - Page 5 ESPA Interface ¾ STPSat-1 is mechanically attached to the... ¾ Separation system attaches to both STPSat-1 and the ESPA with twenty... to the separation system when STPSat-1 was mounted to the ESPA... performed in Aug 2003 with STPSat-1 EDU structure Photograph reprinted courtesy...-5 - Page 7 Secondary Payload Deployment Issues ¾ STPSat-1 was one of five spacecraft... Force. SSC07-VII-5 - Page 9 Conclusion ¾ STPSat-1 was successfully launched on March... site related issues faced by STPSat-1 are likely to be faced...



Дата загрузки: 2017-02-06
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0.09/5
...) • NPSAT1 (Naval Post Graduate School) • STPSat-1 (STP funded with Naval & AF... 35.4º inclination. On-Orbit Operations STPSat-1 and Orbital Express will be... NEXTSat ASTRO Booster Adapter MidSTAR-1 STPSAT-1 FalconSAT-3 ESPA NPSAT1 CFE not... TechSAT-21 CFE TechSAT-21 STPSAT-1 NPSAT1 FalconSAT-3 CFE MidSTAR-1 Delta... Ranking Orbital Express CFESat -- CFE 5 2 STPSat-1 -- SHIMMER 4 -- MEPSI 27 -- CITRIS 24... Space for the Warfighter 10 STPSat-1 STP-owned contract with AeroAstro...



Дата загрузки: 2017-03-09
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0.09/5
... awarded by NASA to AeroAstro. STPSat-1 was developed for the Air... about $3.5 million. HETE cost $4.2 million. STPSat-1 was expected to cost $12... an image of Earth's ionosphere. STPSat-1. This technology demonstration satellite featured... mi Artist's Rendition of the STPSat-1 Source: AeroAstro Variants/Upgrades ALEXIS... follow-on HETE-2 in 2000. STPSat-1. The Department of Defense Space... of other space mission applications. STPSat-1 Development. The Air Force awarded... 2001 to design and build STPSat-1. AeroAstro was also responsible for.... Partners in the construction of STPSat-1 included Northrop Grumman TASC and... Preliminary Design Review of the STPSat-1 spacecraft was completed in July... third quarter of 2003, and STPSat-1 was completed in 2005. The... Secondary Payload Adaptor (ESPA) ring. STPSat-1 was launched in March 2007... was derived largely from AeroAstro's STPSat-1 space vehicle. In March 2010... HETE-2 launched on Pegasus XL STPSat-1 launched on Atlas V JMAPS expected...



Дата загрузки: 2017-04-09
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0.03/5
... Orbital 2007 Express 2000 MTI STPSat-3 STPSat-2 DARPASAT 0 185 2013 2010 1994... flexibility for rapid target selection. STPSat-2 Built for the United States... a Minotaur IV from Kodiak, Ala., STPSat-2, a BCP 100, demonstrates the utility... stars, asteroids, comets and galaxies. STPSat-2 Suomi NPP Launched October 2011... Joint Polar Satellite System (JPSS-1). STPSat-3 Kepler Built in only 47... the United States Air Force, STPSat-3 has repeatedly demonstrated its ability... space. WISE Orbital Express NEXTSAT STPSat-3 The Orbital Express NEXTSAT—or...



Дата загрузки: 2016-11-24
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SSC08-II-3 STPSat-1 – One Year of Successful Operations ... frank.scalici@aeroastro.com ABSTRACT STPSat-1 was launched on March 8, 2007... Force/AeroAstro team completed the STPSat-1 Launch and Early Orbit checkout... data collection. On multiple occasions STPSat-1 has shown robustness in software... the in-orbit history of STPSat-1’s proposed one-year mission life... specifying a quantitative probability of success, STPSat-1 was required to provide a mission... The Space Test Program (STP) STPSat-1 mission was initiated in 2001... the prime contractor for the STPSat-1 space vehicle; both experiments were... (SCC07VII-5) associated with the STPSat-1 mission. Barnisin STPSat-1 was launched on the... as expected in separating the STPSat-1 SV from the ESPA ring... of engine burns and maneuvers, STPSat-1 was successfully released into its.... Figure 1. Illustration of fully-deployed STPSat-1 SV on orbit, with CITRIS... standard separation adapter on back. STPSat-1 on-orbit operations are conducted... (TT&C), and Thermal Subsystem. The STPSat-1 Power Subsystem is a direct-energytransfer... of operation began immediately after STPSat-1 separation from the ESPA ring... the mission operations lead. Figure 2. STPSat-1 Power Simulation Output of Bus... available data indicates that the STPSat-1 Space Vehicle (SV) successfully withstood... the front to backside of STPSat-1’s doublesided deployed solar arrays. The... operations. SHIMMER SHUTTLE RE-POINTING STPSat-1 is a three-axis stabilized, nadir... the star tracker’s field-ofview. STPSat-1 does perform active roll slewing... during the Shuttle’s launch.1 Figure 3. STPSat-1 On-Orbit Bus Power – Solar... were discovered that affected both STPSat-1’s star tracker and GPS (discussed... before the launch of STS117, STPSat-1 was successfully rolled to observe... 10000 12000 ADCS PERFORMANCE Figure 4. STPSat-1 Attitude Pointing Errors in Roll... error is defined in the STPSat-1 Mission Requirements Document to be... this graph, STPSat-1 holds this pointing margin consistently. Figure 5. STPSat-1 ADCS Performance... the star field imaged by STPSat-1’s star tracker, the primary attitude... trackers, etc.). As a Class C spacecraft, STPSat-1 is single string and only... only one star tracker aboard STPSat-1 from which the ADCS software... shows that for those times STPSat-1 has an attitude excursion over... 0.05 deg (within spec). However, STPSat-1 later experienced some radiation hits... in the design phase of STPSat-1 not only for cost considerations...-class satellite. This aspect of STPSat-1 design was extensively discussed and... red dots. GPS Radiation Hits STPSat-1’s GPS receiver provides orbital position... SAA, where STPSat-1’s orbit has substantial exposure. Analysis of STPSat-1’s on-orbit.... POWER PERFORMANCE Power System Description STPSat-1 has a direct energy transfer system... these loads are redundant. Since STPSat-1 has only one star tracker... outages, it was necessary for STPSat-1 to perform a pre-defined 180... variation averaged 161mV. Shunt Anomaly STPSat-1 was originally launched in to...° yaw maneuver was scheduled for STPSat-1 to prevent the star tracker... appears to be “flying backwards.” STPSat-1 then holds this orientation, and... with the power system on STPSat-1. Approximately 6 months after launch, the... described, the solar panels on STPSat-1 are arranged in four deployable... was temporarily commanded to a Figure 9. STPSat-1 battery current over one orbit... of several shunts. However, when STPSat-1 was commanded into CITRIS-Wake... the LEO phase of the STPSat-1 mission, returning valuable science data... operations. Fortunately, the pre-launch STPSat-1 power budget was proven to... hard work contributed greatly to STPSat-1’s successful first year of on... also wish to thank the STPSat-1 mission operations team at KAFB... first year of mission operations, STPSat-1 has successfully achieved mission and...



Дата загрузки: 2016-11-24
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0.09/5
... proverb states. PRIORITY BRIEFING 74 STPSAT-1: Two Years Of Successful Operation..., Patricia Remias, and Frank Scalici STPSat-1 was launched on March 8, 2007... — May 2009 73 PRIORITY BRIEFING STPSat-1: Two Years of Successful Operations... AeroAstro (CAA) team completed the STPSat-1 Launch and Early Orbit checkout... data collection. On multiple occasions STPSat-1 has shown robustness in software... stymied a less robust design. The STPSat-1 mission parameters specified an onorbit... one year. On March 8, 2009, STPSat-1 completed its second year of... SHIMMER and CITRIS payloads, operates STPSat-1 from their Blossom Point facility... Charles County. Missions such as STPSat-1 prove that the “small” satellite... The Space Test Program (STP) STPSat-1 mission was initiated in 2001... the prime contractor for the STPSat-1 space vehicle; both experiments were... specifying a quantitative probability of success, STPSat-1 was required to provide a mission..., over Illustration of fully-deployed STPSat-1 SV on orbit, with CITRIS... presence of on-orbit anomalies. STPSat-1 was launched on the STP... of engine burns and maneuvers, STPSat-1 was successfully released into its... of operation began immediately after STPSat-1 separation from the ESPA ring... available data indicates that the STPSat-1 Space Vehicle (SV) successfully withstood... as expected in separating the STPSat-1 SV from the ESPA ring... tip-off rates observed. The STPSat-1 Power Subsystem is a direct-energytransfer... the front to backside of STPSat-1’s double-sided deployed solar arrays... of GPS position and velocFigure 2. STPSat-1 Power Simulation Output of Bus... star tracker’s field-of-view. STPSat-1 does perform active roll slewing... originally Figure 3. not required) for a STPSat-1 On-Orbit Bus Power – Solar... for SHIMMER to affected both STPSat-1’s star tracker and GPS. Howobserve... expected. SHIMMER Shuttle Re-Pointing STPSat-1 is a three-axis stabilized, nadir... before the launch of STS117, STPSat-1 was successfully rolled to observe... error is defined in the STPSat-1 Mission Requirements Document to be...-launch ADCS perFigure 4. formance simulations STPSat-1 Attitude Pointing Errors in Roll... the star field imaged by STPSat-1’s star dicating close agreement with... requiretrackers, etc.). As a Class C spacecraft, STPSat-1 is single string and only... aboard STPSat-1 from which as can be seen from this graph, STPSat... in the design phase of STPSat-1 not only for cost considerations...-class satellite. This aspect of STPSat-1 design was extensively discussed and... 2009 77 PRIORITY BRIEFING Figure 5. STPSat-1 ADCS Performance One Year after... SAA, where STPSat-1’s orbit has substantial exposure. Analysis of STPSat-1’s on-orbit... 0.05 deg (within spec). However, STPSat-1 later experienced some radiation hits... this anomaly. GPS Radiation Hits STPSat-1’s GPS receiver Figure 6. provides orbital... quickly remedied by limit Since STPSat-1 has only one star tracker.... ages, it was necessary for STPSat-1 to perform a predefined 180-degree... Power Performance Power System Description STPSat-1 has a direct energy transfer system... of several shunts. However, when STPSat-1 was commanded into CITRIS-Wake... dissipation. Fortunately, the pre-launch STPSat-1 power budget was proven to... the LEO phase of the STPSat-1 mission, returning valuable science data... hard work contributed greatly to STPSat-1’s successful first year of on... also wish to thank the STPSat-1 mission operations team at KAFB...