{"projectId":93492,"project":{"projectId":93492,"title":"Flight Demonstration of a Micropump-based Stage Pressurization System","startDate":"2017-06-09","startYear":2017,"startMonth":6,"endDate":"2017-12-08","endYear":2017,"endMonth":12,"programId":73,"program":{"ableToSelect":false,"acronym":"SBIR/STTR","isActive":true,"description":"<p>The NASA SBIR and STTR programs fund the research, development, and demonstration of innovative technologies that fulfill NASA needs as described in the annual Solicitations and have significant potential for successful commercialization. If you are a small business concern (SBC) with 500 or fewer employees or a non-profit RI such as a university or a research laboratory with ties to an SBC, then NASA encourages you to learn more about the SBIR and STTR programs as a potential source of seed funding for the development of your innovations.</p><p><strong>The SBIR and STTR programs have 3 phases</strong>:</p><ul><li><strong>Phase I</strong> is the opportunity to establish the scientific, technical, and commercial feasibility of the proposed innovation in fulfillment of NASA needs.</li><li><strong>Phase II</strong> is focused on the development, demonstration and delivery of the proposed innovation.</li></ul><p>The SBIR and STTR Phase I contracts last for 6 months with a maximum funding of $125,000, and Phase II contracts last for 24 months with a maximum funding of $750,000 - $1.5 million.</p><ul><li><strong>Phase III</strong> is the commercialization of innovative technologies, products, and services resulting from either a Phase I or Phase II contract. 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Candidate small spacecraft which could benefit from dedicated launch services or reduced launch costs provided by the technology include numerous CubeSats and nanosats in development at NASA or funded by NASA, such as NASA's CubeSat Launch Initiative and Educational Launch of Nanosatellites. Other longer term potential applications include future missions to Mars and other bodies which use pressure-fed systems, whether directly or in conjunction with pump-fed engines. For Mars ascent, this technology is particularly attractive when using in-situ propellants since it eliminates the need for a pressurant like helium. The application of this technology for Mars missions is likely to be years away.<br /> <br />With the Vector-R micro-launcher, Vector is positioning itself to provide responsive, dedicated launch to the micro- and nanosat market expected to burgeon in the next few years. Candidate small spacecraft which could benefit from dedicated services or reduced launch costs provided by the technology include commercial entities operating constellations, such Planets (formerly known as Planet Labs) and Google's Terra Bella (formerly known as Skybox Imaging), as well as numerous other CubeSats and nanosats development efforts funded NSF, the Air Force, ORS and SMDC. 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Specifically, the NASA SBIR/STTR Program has the Phase II Enhancement (Phase II-E) and Phase II eXpanded (Phase II-X) contract options.&nbsp;</p><p><strong>Please review the links below to obtain more information on the SBIR/STTR programs.</strong></p><ul><li><strong><a target=\"_blank\" href=\"http://sbir.gsfc.nasa.gov/sites/default/files/ParticipationGuide.pdf\">Participation Guide</a></strong></li></ul><p>Provides an overview of the SBIR and STTR programs as implemented by NASA</p><ul><li><strong><a href=\"http://sbir.gsfc.nasa.gov/solicitations\">Program Solicitations</a></strong></li></ul><p>Provides access to the annual SBIR/STTR Solicitations containing detailed information on the program eligibility requirements, proposal instructions and research topics and subtopics</p><ul><li><strong><a href=\"http://sbir.gsfc.nasa.gov/prg_sched_anncmnt\">Schedule and Awards</a></strong></li></ul><p>Schedule and links for the SBIR/STTR solicitations and selection announcements</p><ul><li><strong><a href=\"http://sbir.gsfc.nasa.gov/content/additional-sources-assistance\">Sources of Assistance</a></strong></li></ul><p>Federal and non-Federal sources of assistance for small business</p><ul><li><strong><a href=\"http://sbir.gsfc.nasa.gov/abstract_archives\">Awarded Abstracts</a></strong></li></ul><p>Search our complete archive of awarded project abstracts to learn about what NASA has funded</p><ul><li><strong><a href=\"http://sbir.gsfc.nasa.gov/content/frequently-asked-questions\">Frequently Asked Questions</a></strong></li></ul><p>&nbsp;Still have questions? 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Candidate small spacecraft which could benefit from dedicated launch services or reduced launch costs provided by the technology include numerous CubeSats and nanosats in development at NASA or funded by NASA, such as NASA's CubeSat Launch Initiative and Educational Launch of Nanosatellites. Other longer term potential applications include future missions to Mars and other bodies which use pressure-fed systems, whether directly or in conjunction with pump-fed engines. For Mars ascent, this technology is particularly attractive when using in-situ propellants since it eliminates the need for a pressurant like helium. The application of this technology for Mars missions is likely to be years away.<br /> <br />With the Vector-R micro-launcher, Vector is positioning itself to provide responsive, dedicated launch to the micro- and nanosat market expected to burgeon in the next few years. Candidate small spacecraft which could benefit from dedicated services or reduced launch costs provided by the technology include commercial entities operating constellations, such Planets (formerly known as Planet Labs) and Google's Terra Bella (formerly known as Skybox Imaging), as well as numerous other CubeSats and nanosats development efforts funded NSF, the Air Force, ORS and SMDC. 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Candidate small spacecraft which could benefit from dedicated launch services or reduced launch costs provided by the technology include numerous CubeSats and nanosats in development at NASA or funded by NASA, such as NASA's CubeSat Launch Initiative and Educational Launch of Nanosatellites. Longer-term potential applications include future missions to Mars and other bodies which use pressure-fed systems, whether directly or in conjunction with pump-fed engines. For Mars ascent, this technology is particularly attractive when using in-situ propellants since it eliminates the need for a pressurant like helium. The application of this technology for Mars missions is likely to be years away.<br /> <br />With the Vector-R micro-launcher, Vector is positioning itself to provide responsive, dedicated launch to the micro- and nanosat market expected to burgeon in the next few years. 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