RFI_tab_data.xlsx
XLSX spreadsheet 15 KB Posted
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Department of the Air Force
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| File | Type | Posted |
|---|---|---|
| Agility_Prime_RFI Update Feb 20.pdf | ||
| VTOL - Request for Information.pdf |
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USAF RFI Technical Data Request
| Response Information | ||||
| Company Name | ||||
| Date | ||||
| Name of Person Completing this form | ||||
| Job / Position Title | ||||
| Telephone Number | ||||
| eMail Address | ||||
| Aircraft Basics | Symbol | Unit | Value | Remarks/Confidence Levels of Data |
| Aircraft Name / Model | ||||
| Length | L | m | ||
| Width | W | m | ||
| Height | H | m | ||
| Wing Span | b | m | ||
| Wing Area | S_w | m^2 | ||
| Horizontal Tail Area | S_ht | m^2 | ||
| Vertical Tail Area | S_vt | m^2 | ||
| Mass Characteristics | Symbol | Unit | Value | Remarks/Confidence Levels of Data |
| Aircraft Mass | M_ac | kg | ||
| Accommodations | N_pers | Seats | ||
| Payload Mass (Crew, Pax, Cargo) | M_PL | kg | ||
| Battery Mass | M_Batt | kg | ||
| Fuel Mass | M_fuel | kg | ||
| Useful Mass (M_PL + M_Batt + M_fuel) | M_UL | kg | ||
| Empty Mass (M_ac - M_UL) | M_e | kg | ||
| Hover Characteristics | Symbol | Unit | Value | Remarks/Confidence Levels of Data |
| Number of Lift Propellers | Nr_lift | - | ||
| Propeller Diameter | D_lift | m | ||
| Propeller RPM | RPM_hov | RPM | ||
| Disk Loading at M_ac | DL | N/m^2 | ||
| Power to Hover at M_ac (IGE) | P_hov | kW | ||
| Power to Hover at M_ac (OGE) | P_hov | kW | ||
| Aircraft Figure of Merit | FM_ac | - | ||
| Lift Motor Torque | Q_lft | N.m | ||
| Lift Motor Specific Torque | Q_sp_hov | N.m/kg | ||
| Cruise Characterisits | Symbol | Unit | Value | Remarks/Confidence Levels of Data |
| Number of Cruise Propellers | Nr_cru | - | ||
| Propeller Diameter | D_cru | m | ||
| Cruise Speed at M_ac | V_cru | kt | ||
| Propeller RPM at V_cru | RPM_cru | RPM | ||
| Lift/Equiv_Drag at V_cru | L/De_cru | - | ||
| Power at V_cru, M_ac | P_cru | kW | ||
| Best Endurance Speed at M_ac | V_be | kt | ||
| Propeller RPM at V_be | RPM_be | RPM | ||
| Lift/Equiv_Drag at V_be | L/De_be | - | ||
| Power at V_be, M_ac | P_be | kW | ||
| Cruise Motor Torque | Q_cru | N.m | ||
| Cruise Motor Specific Torque | Q_sp_cru | N.m/kg | ||
| Wing Loading at M_ac | WL | N/m^2 | ||
| Electrical Characteristics | Symbol | Unit | Value | Remarks/Confidence Levels of Data |
| Electric Chemistry Type | ||||
| Number of Battery Packs | N_BP | - | ||
| Energy per Battery Pack | E_BP | kW.h | ||
| Mass of Each Battery Pack | M_BP | kg | ||
| Specific Energy of Battery Pack | E_sp_BP | kW.h/kg | ||
| Specific Energy of Cell | E_sp | kW.h/kg | ||
| Battery Discharge Rate | C | 1/h | ||
| Battery Recharge Rate | C | 1/h | ||
| Operating Voltage | V | V | ||
| Operating Current | I | A | ||
| Usable Energy | e_use | kW.h | ||
| Reserve Energy | e_res | kW.h | ||
| Electrical System Efficiency | e_eff | - | ||
| Battery Charger Model and Specs. | ||||
| Fuel Propulsion Characteristics | Symbol | Unit | Value | Remarks/Confidence Levels of Data |
| Engine Model | ||||
| Engine Type | ||||
| Fuel Chemistry / Type | ||||
| Fuel Density | rho_fuel | kg/m^3 | ||
| Engine Installed Power | P_inst | kW | ||
| Engine SFC | SFC_eng | kg/kW.h | ||
| Fuel Capacity | f_vol | l | ||
| Useable Fuel | f_use | l | ||
| Reserve Fuel | f_res | l | ||
| Mission Characteristics (Provide Graphical & Tabulated Time Data of the Following) | Remarks/Confidence Levels of Data | |||
| Mission Profile / Segments | MX = f(t) | - | Please provide as graphs and/or tabulated data on separate sheet(s) | |
| Power Profile | P = f(t) | kW | ||
| Translational Speed | Vx = f(t) | kt | ||
| Vertical Speed | Vy = f(t) | m/s | ||
| Height AGL | H = f(t) | m | ||
| C-Rate | C = f(t) | 1/h | ||
| Electrical Energy Remaining | E = f(t) | kW.h | ||
| Fuel Remaining | F = f(t) | kg | ||
| Battery Temperature | T = f(t) | deg. C | ||
| Distance Travelled | S = f(t) | m |
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