US Army Space and Missile Defense Command Operational Nanosatellite Effect (SMDC-ONE)

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    US ArmySpace and Missile Defense Command

    Operational Nanosatellite Effect (SMDC-ONE)

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    System ConfigurationSMDC-ONE

    Spacecraft Segment

    Bus

    Element

    Guidance Nav

    & Control

    Structures &

    Mechanical

    Thermal

    Control

    Command &

    Data Handling

    Electrical

    Power

    Comm

    Element

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    Mission Objectives

    1. Demonstrate the ability to rapidlydesign and develop militarily relevant

    low cost spacecraft.

    2. Primary Operational Objectivea. Scenario OV-1. Receive packetized

    data from multiple Unattended GroundSensors (UGS). Transmit that data toground stations within the SMDC-ONEground track.

    3. Secondary Operational Objectivea. Scenario OV-2. Provide real time voice

    and text message data relay to andfrom field deployed tactical radiosystems.

    4. Demonstrate SMDC-ONE operationallife time of 12 months or longer.

    Mission Objectives

    1. Design, develop, and deliver eightSMDC-ONE satellite systems within 12

    months of ATP (April 2008) for ahardware cost not to exceed $350k persatellite.

    2. Receive UGS signal on two or moreSMDC-ONE satellites and successfully

    relay that signal to a deployed groundstation.*

    3. Not required for mission success.

    4. Demonstrate an on-orbit operationallife of 6 months or longer.**

    Minimum Success Criteria

    Dependent upon launch of 8 satellites** Dependent upon assigned orbit

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    Design Reference Mission

    Falcon 1 launch east fromKwajalein Atoll

    Stage 1 BO169 sec

    Orbital Insertion~400 km450 sec

    Stage 1 Impact

    VehicleOrient

    Begin SMDC-ONEDeployment Phase

    7.5 min

    Nanosat Deploy (8)

    Circularization

    Burn~ 52 min

    45 min

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    Primary Mission OV-1 CONOP

    Satellite-Autonomous Data Collectionfrom Unmanned Ground Sensor (UGS)Segments

    Mission Executed From Stored Scheduleror C2 Uplink Instructions 1 Based onTime Schedule

    Satellite Polls Pre-Loaded UGS ID # 2on Ground and Retrieves Data

    Satellite Data Collection from UnmannedGround Sensors (UGS) 3

    Collected UGS Data Transferred to Ground4

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    Status as of April 23

    Spacecraft Critical Design Review Completed in

    December 2008 Spacecraft Radio Frequency pattern/strengthtesting completed at AMRDEC UnconventionalBeam Office test facility -- Redstone Arsenal,Huntsville.

    Spacecraft Integration and Functional Tests areunderway.

    Environmental Test Series Shock test at Marshall Space Flight Center

    Vibration testing at Miltec Iuka, MS facility

    Thermal Balance / Thermal Cycling at MiltecHuntsville facility

    US Army Acceptance April 28 at Miltec facility 8 flight units

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    Verification Testing

    Shock test at MSFC on two qualificationunits.

    Random Vibration performed at MiltecIuka facility on qual and flight units

    Thermal Balance testing performed onsingle qual unit as part of thermalcycling test to verify on-orbit predictions

    Thermal Cycling under vacuum on qual

    and flight units Antenna Deployment Test performed as

    part of thermal vacuum testing

    Antenna Pattern verification to beperformed at Redstone Arsenal Armyfacility using specially designed RF

    mock-up Planning for end-to-end RF test at

    Redstone Arsenal following delivery.

    Shock Test NASA MSFC

    Vibe Test Miltec Iuka

    Thermal Balance / Thermal CyclingMiltec Huntsville

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    Virtual Tour

    SLA Model

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    Virtual Tour