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


Дата загрузки: 2016-12-09
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0.11/5
... 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: 2017-06-14
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0.22/5
... in the Strategic Intent document, STPSat-2 and ORS-1. MMSOC GSA provides... mission unique GS requirements. The STPSat-2 program will be the first... that of the 99 total STPSat-2 GS requirements (found in the... directly used to verify 40 STPSat-2 requirements, leaving only 59 mission... requirements to be verified through STPSat-2 testing. Assuming a relatively even distribution... required to test the 59 STPSat-2 Mission Unique (MU) GS requirements... 9, the overlapping requirements saved the STPSat-2 program over 4080 man hours... overlap between MMSOC GSA and STPSat-2 MU GS. The resulting time... the overall test schedule for STPSat-2. The ORS-1 Program Office and... testing similar to that of STPSat-2. ORS-1 will be able to... after STPSat-2, the successful test results and operational performance of the STPSat...” was developed for use on STPSat-2. The objective of the program... example, the bus structure of STPSat-2 (SIV-1), was subjected to qualification... as the spacecraft bus of STPSat-3. Since SIV-2 has an identical...-2 allowed the test schedule for STPSat-3 to be accelerated without reducing... and SV programs. (Top left: STPSat-2, Top Right ORS-1, Bottom Left... from earlier missions such as STPSat-2 and TacSat-3, with adjustments based... short period of time. The STPSat-2 program used test plans, test... effort. As mentioned previously, ORS-1, STPSat-2 and SIV-2 have all leveraged... wherever possible within ORS-1 and STPSat-2 by allowing the eventual users... be combined with training events. STPSat-2 proved this concept by combining... been demonstrated in MMSOC, ORS-1, STPSat-2 and SIV-2. As these systems... Architecture Strategic Intent”; April 2009 8 STPSat-2 Ground Specification Document (GSD), 04..., Development and Sustainment, TO 0048 STPSat-2 Phase II Ground Segment Development..., Requirement Verification; (TO48_Ph2_Test_BOE.xls) 10 STPSat-2 Preliminary Design Review Presentation; (02_Requirements...



Дата загрузки: 2016-12-09
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0.1/5
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: 2017-06-15
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0.06/5
... STPS26 mission include FalconSat-5, FASTRAC, STPSat-2, O/OREOS, and RAX [?]. Figure 21... 2-1. STPSat-2 is an ESPA class satellite built by Ball Aerospace [7]. STPSat-2 carries... terrestrial sensors to users” [14]. STPSat-2 is the first satellite to... its attitude to within 0.1 degrees. STPSat-2 is shown on the far....html, August 2005. [7] “Ball Aerospace STPSat-2 Satellite Launches Aboard STP-S26...’s Space Page: STPSat-2”. http://www.skyrocket.de/space/doc_sdat/ stpsat-2.htm, 2011...



Дата загрузки: 2016-12-29
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0.08/5
... 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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0.13/5
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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0.11/5
...) • 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: 2017-06-14
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0.24/5
Press Release FOR IMMEDIATE RELEASE MSCI IS PLEASED TO NOTE THE SUCCESSFUL LAUNCH OF THE UNITED STATES AIR FORCE STPSAT-2 Mississauga, Ontario – November 22, 2010 – Microsat Systems Canada Inc. (MSCI) (formerly the Space Division of Dynacon Inc.), Canada’s designer and builder of the Multi Mission Microsatellite Bus technology, and innovator of MicroWheel (reaction wheel) attitude control systems, is pleased to note the successful launch of the United States Air Force STPSat-2 at 8:25 GMT November 20, 2010 out of Alaska’s Kodiak Launch Complex. STPSat-2 was released at an altitude of 400 miles from a Minotaur 4 rocket and placed into a polar orbit. At 10:45 PM GMT the spacecraft’s primary payload radioed back to Earth through a ground station in Hawaii that its solar panels had been extended and that it was operating normally. The heart of the STPSat-2 attitude control system is three of MSCI’s MW 1000 Reaction Wheels. The STP S26 mission is being conducted by the United States Air Force Space Test Program, the military's research and development wing responsible for flight opportunities for emerging technologies. STPSat-2 is the second spacecraft in the Space Test Program Standard Interface Vehicle (STP-SIV) program. Col. Michael Moran is the mission director for this launch. "Since 1965, the Space Test Program has been an invaluable service to our nation by flying science and technology payloads that are fundamental to the DOD's approach to space acquisition and to the advancement of our nation's space capabilities," Moran said. "Extraordinary military capabilities, such as military satellite communications and the Global Positioning System, can trace their development back to earlier Space Test Program missions. Enabling technologies for those systems were incrementally demonstrated in the space environment by the spaceflight opportunities provided by STP.i" Press Release Picture courtesy of ballaerospace.com MSCI worked with attitude control system lead Comtech AeroAstro to provide the three (3) MW 1000 Reaction Wheels to STPSat-2 prime contractor Ball Aerospace in 2008. “The Space Test Program’s Standard Interface Vehicle (STP-SIV) project has developed a common spacecraft bus with a standard payload interface to accelerate Department of Defense space technology and ensure future U.S. space superiority.ii” says Ball Aerospace “Payload teams are able to design payloads and specific experiments to be compatible with the flexible standardized vehicle, resulting in lower spacecraft non-recurring costs and increased spaceflight opportunities. By providing such a vehicle, the Space Test Program can shorten acquisition timelines and decrease spacecraft build.iii” Although MSCI has provided Reaction Wheels to customers around the world for a number of years, this was the first program with a USAF spacecraft since the TACSAT2 mission to carry MW 1000’s. Since this STPSat-2 mission, MSCI has also delivered an additional three (3) Reaction Wheels for the STPSat-3 mission. “The STP program and our close relationship with Ball Aerospace are very important to us,” states David R. Cooper, MSCI’s President and CEO. “Our trusted position on Ball’s STP standardized bus team provides additional validation of the industry’s confidence in MSCI’s Reaction Wheels, a position we value and must continue to earn with each new contract. Our congratulations to David Kaufman and the entire Ball Aerospace team.” About MSCI MSCI is Canada’s leader in the design, development and delivery of cost-effective microsatellites, and the developer of Canada’s Multi Mission Microsatellite Bus technology (MMMB), capable of hosting a wide variety of remote sensing, communications, scientific and military payloads. MSCI also has proven capabilities in Press Release systems engineering analysis, the development of sophisticated, cost-effective Reaction Wheel attitude control systems solutions and their implementation into flight hardware and software. Formerly the Space Division of Dynacon Inc., MSCI has been the premiere builder of microsatellites in Canada for over a decade. MSCI provides military and civil space agencies, as well as commercial markets, with space technology that enables space exploration and surveillance of Earth from space and other services for commercial applications. Additional information about MSCI can be found at www.mscinc.ca. Additional information about MSCI’s MicroWheel (reaction wheel) attitude control systems can be found at www.reactionwheel.com. For more information, please contact: Justin Phillips Vice President, Marketing Microsat Systems Canada Inc. (MSCI) (647) 285-0442 justin.phillips@mscinc.ca ### i http://live.spaceflightnow.com/stps26status.html http://www.ballaerospace.com/page.jsp?page=126 iii http://www.ballaerospace.com/page.jsp?page=126 ii



Дата загрузки: 2017-03-09
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0.1/5
... 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...