Attachment_L-1_-_Vol_2_AVP_Data.xlsx

XLSX spreadsheet 14 KB Posted

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Unmanned Aircraft Systems Intelligence, Surveillance, and Reconnaissance (UAS ISR) Services
Solicitation number
FA4890-17-R-0015
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Attachment L-1 - Vol 2 AVP Data (Updated)

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FA4890-17-R-0015-0005.docx DOCX document
Amend_0004_-_Remaining_Questions-Recommendations.docx DOCX document
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FA4890-17-R-0015-0003.pdf PDF
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Attachment_1_-_PWS_-_UAS_ISR_--_8_Dec_17.pdf PDF
FA4890-17-R-0015-0002.docx DOCX document
Attachment_L-1_-_Vol_2_AVP_Data.xlsx XLSX spreadsheet
Amend_0002_-_Questions_and_Responses.docx DOCX document
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FA4890-17-R-0015-0001.pdf PDF
Attachment_L-1_-_Vol_2_AVP_Data.xlsx XLSX spreadsheet
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Attachment_2a_-_DD254_continuation_-_UAS_ISR.docx DOCX document
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FA4890-17-R-0015.docx DOCX document
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Text version

Sheet1

Clearly identify the location of each item below within the test report for the mission profile flight.
REQUIREMENTVALUEPAGEPARAGRAPH #
HardwareFuselageModel / SN
EO PayloadModel / SN
NIIRS
IR PayloadModel / SN
NIIRS
Radio RelayDimensions (LxWxH)
Volume (in3)
Weight (lbs)
Power (W)
WingModel / SN
EmpennageModel / SN
AntennaModel / SN
CommunicationsModel / SN
PropellerModel / SN
EngineModel / SN
FuelFuel type
Fuel Loading (lbs)
Fuel Burn Rate (lbs/hr)
Fuel Remaining
EnvironmentalWind (knots)
Temperature (°F)
Density Altitude
Airspeed (knots)Cruise
Dash/maximum
Altitude (feet AGL)
Datalink Range (NM)
Endurance (hours)
Configuration GeometryDimensioned Three View
Layout and placement of internal components
Component wetted areas
Propeller description
Engine
Aero / PerformanceZero-lift drag buildup
Cruise Drag Polar
Installed takeoff thrust
Cruise thrust available as function of flight speed
Cruise Fuel Burn rate (lbs/hr)
Mass PropertiesComponent weights / Aircraft center of gravity
Variations with payload options and fuel burn

N00019-16-R-0063 Attachment (L-7)

Sheet2

Sheet3

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