N a S a Fa C Ts

National Aeronautics and Space Administration Fast, Affordable, Science and Technology SATellite (FASTSAT) Microsatellite FASTSAT is NASA’s first microsatellite designed FASTSAT establishes a platform and environment to create a capability that increases opportunities where science and technology research experiment for secondary, scientific and technology payloads, payloads of low- and mid-level complexity can be or rideshares, to be flown at lower cost than flown responsively and affordably in low-Earth orbit previously possible. The FASTSAT microsatellite design supports the The overall objective of the FASTSAT mission is standards of the Evolved Expendable Launch Vehicle to demonstrate the capability to build, design and Secondary Payload Adaptor, or ESPA – an adapter facts test a microsatellite platform to enable govern- ring developed by the U.S. Department of Defense, mental, academic and industry researchers to or DoD, specifically for accommodating secondary conduct low-cost scientific and technology exper- spacecraft launch opportunities. iments on an autonomous satellite in space. Such research is intended to support NASA’s Science Mission Directorate and Exploration Systems Mission Directorate, led by NASA Headquarters in Washington. NASA The FASTSAT spacecraft bus outfitted with six payloads. Credit: NASA The Mission Mission Profile Gaining access to space is a costly endeavor with limited FASTSAT is one of three secondary microsatellites payloads opportunities for small launch payloads. Delayed access to approved to fly on a Minotaur IV launch vehicle built and oper- space impacts science and technology research that could ated by Orbital Sciences Corporation, to be launched from the bring advancements or solutions to real-world problems. Alaska Aerospace Development Corporation’s Kodiak Launch Complex on Kodiak Island, Alaska. FASTSAT, leveraging the ESPA ring, will allow multiple users opportunities to conduct research on numerous launch vehi- Outfitted with six technology and atmospheric experiments, cles in space at lower cost and with greater frequency than FASTSAT will lift off from Kodiak in late fall 2010. Approximately previously possible. 20 minutes after launch, FASTSAT will separate from the launch vehicle for orbital insertion. Thirty minutes later, FASTSAT will The ESPA ring mounts up to six, 400-pound secondary satellites automatically power up to begin initial checkout operations. to “share a ride to space” with an additional primary payload up to 15,000 pounds. The ESPA ring attaches between the primary Within one hour after launch, FASTSAT will separate from the payload and the expendable upper stage on an Atlas V or Delta launch vehicle. The Marshall Center will contact the spacecraft IV. ESPA provides a “virtually free” ride for ESPA-class satellites and begin on orbit operations. For the first 11 days after launch, and increased opportunities for launch ridesharing with DoD the spacecraft and the experiments will go through an on-orbit ESPA configurable launch vehicles for science and technology commissioning phase. experiments. Once commissioning is complete, the next 180 days are The FASTSAT project began in late 2008, when NASA’s Marshall focused on science operations. A checkout and performance Space Flight Center in Huntsville, Ala., and the Department of analysis of each science instrument will be performed and then Defense Space Test Program at the Space Development and one by one each experiment will turn on to perform its science Test Wing at Kirtland Air Force Base, N.M., formed a partner- objectives. After the science phase is complete, additional ship to develop a high risk, low-cost technology demonstration characterization of the spacecraft will be performed to test experiment. The development pace was fast because the Space additional flight objectives. The experiments will be performed Test Program had received notification just 14 months prior to in parallel to test the overall abilities of the spacecraft. This will launch that a secondary payload had been cancelled on the last approximately 100 days. After completion of this phase of STP-S26 mission, opening up a 25-percent payload vacancy. the mission, the command will be sent to shut down the spacecraft, which will go into a decommissioning phase. FASTSAT was selected as an “outside the box” solution that afforded a highly synergistic concept which satisfied experi- Mission control for FASTSAT and its onboard experiments ment, payload and launch schedule requirements. The micro- will be managed from the small satellite mission control room satellite was designed, assembled and tested in-house at the at the Marshall Center’s Huntsville Operations and Science Marshall Center using off-the-shelf commercial hardware by Control Center. Experiment operations also will be performed NASA and a group of industry partners. using the control center’s capabilities for managing remote science operations by investigators at their own facilities. FASTSAT will serve as a scientific laboratory platform contain- ing all the resources needed to carry out scientific and technol- Spacecraft Overview: ogy research operations for the mission time period. FASTSAT FASTSAT enables both NASA and military opportunities and all six experiments have successfully passed all phases to conduct innovative research missions that gain unique of ground development and test operations in preparation scientific insights or mature the readiness of new technol- for launch to low-Earth orbit, and have been approved by the ogy components, subsystems or systems by increasing the Department of Defense’s Space Experiments Review Board, a Technology Readiness Level for future missions. FASTSAT group of defense organizations and NASA personnel assigned was developed with a simplicity in the design of the space- to maintain the defense department’s experiment priority list. craft subsystems that provide power management, onboard Potential space experiments are reviewed and ranked by prior- storage of experiment data, control of experiments, communi- ity. The highest ranking experiments are flown by the Space cations with ground stations, propellantless mechanisms Test Program as budget and resources permit. for attitude control and a GPS system for navigation. FASTSAT 2 NASA Facts Miniature Star Tracker (MST) NanoSail-D deployer subsystem Miniature Imager for Neutral Ionosheric atoms and Magnetospheric Electrons (MINI ME) Threat Detection System (TDS) Plasma Impedance Thermospheric Spectrum Analyzer (PISA) Temperature Imager (TTI) Experiments Overview: Threat Detection System and Miniature Star Tracker NanoSail-D The Threat Detection System NanoSail-D is designed to and the Miniature Star Tracker demonstrate deployment of are managed by the Air Force a compact solar sail boom Research Laboratory at Kirtland system that could lead to Air Force Base. further development of NanoSail-D stowed Miniature Star Tracker this alternative propulsion The objective of the Threat Detection System is to evaluate tech- technology and FASTSAT’s niques for measuring the atmospheric propagating characteristics ability to eject a nanosatel- on coherent light generated from known ground stations. lite from a microsatellite – while avoiding re-contact Star Tracker Lens Camera with the FASTSAT satellite bus. NanoSail-D, managed Sunshade by the Marshall Center, will be the first NASA solar sail NanoSail-D deployed deployed in low Earth orbit. Lens Holder NanoSail-D was designed and built by NASA engineers Transmission Grating Camera Holder at Marshall, in collaboration with the Nanosatellite Missions Threat Detection System Office at NASA’s Ames Research Center in Moffett Field, Calif., and Nexolve located in Huntsville. The experiment The FASTSAT spacecraft carries three atmospheric instru- is a combined effort between the U.S. Air Force Research ments built at NASA’s Goddard Space Flight Center in Laboratory at Kirtland Air Force Base, N.M., NASA and the Greenbelt, Md., in partnership with the U.S. Naval Academy U.S. Army Space and Missile Defense Command and the in Annapolis, Md. The instruments include the Thermosphere Von Braun Center for Science & Innovation, both in Huntsville. Temperature Imager, designed to measure remotely the FASTSAT 3 NASA Facts temperature, atomic oxygen and molecular nitrogen densities of the thermosphere; the Miniature Imager for Neutral Iono- spheric Atoms and Magnetospheric Electrons, a low-energy neutral atom imager that will detect neutral atoms formed in the plasma population of the Earth’s outer atmosphere to improve global space weather prediction; and the Plasma and Impedence Spectrum Analyzer, a device that will test a new measurement technique for the temperature and density of Plasma and Impedence Spectrum Analyzer thermal electrons in the ionosphere – which can interfere with radio-based communications and navigation. The Plasma and Impedance Spectrum Analyzer will test a new measurement technique for the thermal electron populations in Thermosphere the ionosphere, calculating their density structuring, which can Temperature Imager interfere with or scatter radio signals used for communication and navigation. The analyzer will determine when and where the The Thermospheric ionosphere becomes structured or turbulent, permitting better Temperature Imager predictive models of space weather effects on GPS signals. will provide the first global-scale measure- The FASTSAT Team ments of thermospheric temperature profiles in FASTSAT will fly on the

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