TE-03 Worksheet in EPFD-01-03.xlsx

XLSX spreadsheet 37 KB Posted Apr 8, 2021

Attached to: Electrified Powertrain Flight Demonstration Federal contract opportunity
Solicitation number: 80AFRC21R0009
Issued by: National Aeronautics and Space Administration Armstrong Flight Research Center

About this file

Written by GovTribe AI · Dec 27, 2023

This document contains technical specifications and requirements for an integrated MW-class electrified powertrain flight demonstration system. Key details include requirements for an electrified powertrain to be ground tested and flight demonstrated, with metrics provided for components, subsystems, vehicle sizing and performance, and operational capabilities. Technical performance parameters are outlined at various stages of review from proposal through critical design and flight readiness reviews. The integrated powertrain system is to be demonstrated on a vision vehicle and must meet metrics for power levels, efficiency, weight, and other characteristics at set review points. The related federal contract opportunity posted by NASA Armstrong Flight Research Center seeks proposals for contracts to develop, test, and fly such an electrified powertrain demonstration system.

View the file

Other files for this federal contract opportunity

Other files attached to Electrified Powertrain Flight Demonstration, newest first.
File	Type	Posted
Domestic or Foreign End Product - Components.xlsx	XLSX spreadsheet	May 3, 2021
80AFRC21R0009P00003.pdf	PDF	May 3, 2021
EPFD-01-03 Integrated Data Requirements Description Document.pdf	PDF	May 3, 2021
EPFD-01-03 Integrated Data Requirements Description Document.pdf	PDF	Apr 16, 2021
AFOP-8715.3-005-2.pdf	PDF	Apr 8, 2021
Industry Day Presentation.pdf	PDF	Apr 8, 2021
TE-02 Worksheet in EPFD-01-03.xlsx	XLSX spreadsheet	Apr 8, 2021
AFOP-7900.3-023.pdf	PDF	Apr 8, 2021
AFOP-8730.5-007-2.pdf	PDF	Apr 8, 2021
80AFRC21R0009P00002.pdf	PDF	Apr 8, 2021
EPFD-02-06 Technical Measures of Effectiveness-Rev B .pdf	PDF	Apr 8, 2021
Industry Day Questions and Answers.pdf	PDF	Apr 8, 2021
80AFRC21R0009P00001.pdf	PDF	Mar 19, 2021
EPFD-01-03 Integrated Data Requirements Description Document Final.pdf	PDF	Feb 23, 2021
EPFD_01_03_Integrated Data Requirements Description Document.pdf	PDF	Feb 22, 2021
80AFRC21R0009.pdf	PDF	Feb 22, 2021
EPFD Statement of Objectives.pdf	PDF	Feb 22, 2021
EPFD-02-02 System Requirements Document.pdf	PDF	Feb 22, 2021
EPFD-02-06 Technical Measures of Effectiveness.pdf	PDF	Feb 22, 2021
EPFD Industry Day QAs.pdf	PDF	Jan 29, 2021
EPFD Industry Day-Public Webinar QAs.pdf	PDF	Jan 29, 2021
EPFD Pre-solicitation Industry Day Slides Final 12.10_with all updates_12_15_2020pptx.pdf	PDF	Dec 18, 2020
EPFD Public Webinars December 11_2020_final__updated_12_15_2020.pdf	PDF	Dec 18, 2020
Draft_EPFD Programmatic Data Requirement Deliverables.pdf	PDF	Dec 9, 2020
Small Business Subcontracting Goals.pdf	PDF	Dec 9, 2020
Draft_EPFD Technical Data Requirement Deliverables.pdf	PDF	Dec 9, 2020
EPFD_02_02_SRD-DRAFT-REV A-20201130.pdf	PDF	Nov 30, 2020
Draft EPFD-02-06 Technical Measures of Effectiveness Preliminary.pdf	PDF	Nov 30, 2020
DRAFT RFP 80AFRC21R0009.pdf	PDF	Nov 20, 2020
DRAFT Statement of Objectives.pdf	PDF	Nov 20, 2020
Notice of Contract Action.pdf	PDF	Oct 22, 2020

Show all 31

On GovTribe

Work with this file on GovTribe

Download the original file
Contacts named in this file
Similar government files
Ask GovTribe AI about this file

Try for free Login

Text version

The file's text, extracted by GovTribe without its formatting.

Vision Vehicle

Vision Vehicle Description
Vision Vehicle Powertrain Architectural Schematic	Vision Vehicle
image here	image here

Vision Vehicle KPPs	At Proposal submission (Units)	SRR (Units)	PDR (Units)	CDR (Units)	FRR (Units)	PFAR (Units)	Mean/Standard Deviation/Delta (Units)	Major Actionable Events - Significant series of events such as tests that may occur in between life cycle reviews and its completion triggers an assessment of TPMs as required per DRD-TE-03: Technical Data Requirements and Reporting
								Component and Subsystem Ground Test(s)	Integrated Ground Test(s)
1. Total Power level of the Integrated MW-Class Powertrain System
2. Power Level of individual electrical components
3. Operating Voltage of the Integrated MW-Class Powertrain System
4. Altitude Capability of the Integrated MW-Class Powertrain System
5. Specific Power of the Integrated MW-Class Powertrain System
6. End to End loss of the Integrated MW-Class Powertrain System
7. Mission Fuel Burn/Energy Reduction
Propulsion Architecture Metrics	At Proposal submission (Units)	SRR (Units)	PDR (Units)	CDR (Units)	FRR (Units)	PFAR (Units)	Mean/Standard Deviation/Delta (Units)	Major Actionable Events
								Component and Subsystem Ground Test(s)	Integrated Ground Test(s)
Specific Power (kW/kg or hp/lbm)
Thrust Specific Power Consumption (W/N or hp/lbf)
Increment Efficiency due to Aero-propulsive (-)
Global Chain Efficiency (-)
Typical Mission Profile	Duration (min)	Length (nm)	Power Management, Allocation and Control Strategy

Stage Length
Gate
Taxi-out
Take-off
Climb
Cruise
Descent
Approach
Landing
Taxi-in
Holding/Loiter
Contingency
Diversion
Vision Vehicle Weights	At Proposal submission (Units)	SRR (Units)	PDR (Units)	CDR (Units)	FRR (Units)	PFAR (Units)	Mean/Standard Deviation/Delta (Units)	Major Actionable Events
								Component and Subsystem Ground Test(s)	Integrated Ground Test(s)
Maximum Take-Off Weight (kg or lbm)
Maximum Landing Weight (kg or lbm)
Manufacturer’s Weight Empty, Green (kg or lbm)
Operating Weight Empty or Basic Oper. Weight (kg or lbm)
Maximum Payload Weight (kg or lbm)
Maximum Zero-Fuel Weight (kg or lbm)
Total Release Energy Weight (kg or lbm)
Release Fuel Weight (kg or lbm)
Release Ancillary Energy Source Weight (kg or lbm)
Vision Vehicle Sizing Parameters and Metrics	At Proposal submission (Units)	SRR (Units)	PDR (Units)	CDR (Units)	FRR (Units)	PFAR (Units)	Mean/Standard Deviation/Delta (Units)	Major Actionable Events
								Component and Subsystem Ground Test(s)	Integrated Ground Test(s)
Wing Loading (kg/m2 or lbm/sq.ft)
Reference Wing Area (m2 or sq.ft)
Reference Wing Aspect Ratio (-)
Disc Loading (kg/m2 or lbm/sq.ft)
Reference Disc Area (m2 or sq.ft)
Number of Rotors and Number of Blades for each Rotor (-)
Maximum Mechanical Speed (RPM)
MWE / MTOW (-)
OWE (BOW) / MTOW (-)
OWE (BOW) / PAX (kg/PAX or lbm/PAX)
Release Energy Weight / MTOW (-)
MLW / MTOW (-)
Conditions Describing Total Maximum Thrust or Power
Total Maximum Thrust (kN or lbf)
Total Maximum Shaft Power (kW or hp)
All-Engines Operational Thrust-to-Weight (-)
One-Engine Inoperative Thrust-to-Weight (-)
AEO Maximum Power-to-Weight (kW/kg or hp/lbm)
AEO Maximum Power Loading (kg/kW or lbm/hp)
OEI Maximum Power-to-Weight (kW/kg or hp/lbm)
OEI Maximum Power Loading (kg/kW or lbm/hp)
Anti-torque or Tail Rotor Power (kW or hp)
Vision Vehicle Operational Performance	At Proposal submission (Units)	SRR (Units)	PDR (Units)	CDR (Units)	FRR (Units)	PFAR (Units)	Mean/Standard Deviation/Delta (Units)	Major Actionable Events
								Component and Subsystem Ground Test(s)	Integrated Ground Test(s)
Take-off Field Length, MTOW, ISA, SL (m or ft)
TOFL (m or ft)
Payload (kg or lbm)
Take-off Gross Weight (kg or lbm)
Specified ISA Deviation (C or F)
Specified Airport Elevation, AGL (ft)
Stall Speed and Flap Setting, MTOW, ISA, SL (KCAS)
Reference Speed and Flap Setting, MLW, ISA, SL (KCAS)
Landing Field Length, MLW ISA, SL (m or ft)
ICAO Cumulative Noise Margin to Chapter 14 (EPNdB)
ICAO NOx-Emissions Level (g/kN)
LTO NOx-Emissions (kg/LTO)
ICAO Metric Value MVCO2 (kg/km.mn)
Maximum Operating Altitude (ft)
Maximum Hover Altitude (ft)
Glide Ratio (nm/ft)
Maximum Endurance Speed (KCAS [KTAS])
Maximum Endurance Time (h)
Climb Speed Schedule (KCAS [Mach])
Maximum Rate-of-Climb, MTOW b.r., ISA, SL (fpm)
Rate-of-Climb, MTOW b.r., ISA (fpm)
Specified Altitude (ft)
Time-to-Climb to Initial Cruise Altitude (min.)
Vision Vehicle Max. PAX/Payload Design Range	At Proposal submission (Units)	SRR (Units)	PDR (Units)	CDR (Units)	FRR (Units)	PFAR (Units)	Mean/Standard Deviation/Delta (Units)	Major Actionable Events
								Component and Subsystem Ground Test(s)	Integrated Ground Test(s)
PAX
Range (nm)
Payload (kg or lbm)
Block Fuel (kg or lbm)
CO2-Emissions (kg or lbm)
Block Fuel per PAX (kg/PAX or lbm/PAX)
CO2-Emissions per PAX (kg/PAX or lbm/PAX)
[Fuel] Specific Air Range (nm/kg or nm/lbm)
Block Energy (MW.h or BTU)
Block Energy per PAX (MW.h/PAX or BTU/PAX)
Degree-of-Hybridization for Block Energy (-)
Energy Specific Air Range (nm/kW.h or nm/BTU)
Miss. Energy Index (kW.h/kg.nm or BTU/lbm.nm)
Operating Economics Assumptions
Operating Cost (USD)
Operating Cost per PAX (USD/PAX)
Vision Vehicle Max. PAX/Payload Off-Design Stage Length	At Proposal submission (Units)	SRR (Units)	PDR (Units)	CDR (Units)	FRR (Units)	PFAR (Units)	Mean/Standard Deviation/Delta (Units)	Major Actionable Events
								Component and Subsystem Ground Test(s)	Integrated Ground Test(s)
PAX
Stage Length (nm)
Payload (kg or lbm)
Block Fuel (kg or lbm)
CO2-Emissions (kg or lbm)
Block Fuel per PAX (kg/PAX or lbm/PAX)
CO2-Emissions per PAX (kg/PAX or lbm/PAX)
[Fuel] Specific Air Range (nm/kg or nm/lbm)
Block Energy (MW.h or BTU)
Block Energy per PAX (MW.h/PAX or BTU/PAX)
Degree-of-Hybridization for Block Energy (-)
Energy Specific Air Range (nm/kW.h or nm/BTU)
Miss. Energy Index (kW.h/kg.nm or BTU/lbm.nm)
Operating Cost (USD)
Operating Cost per PAX (USD/PAX)
Vision Vehicle Components and Subsystems
Engine	SI Units	Imperial Units	At Proposal submission (Units)	SRR (Units)	PDR (Units)	CDR (Units)	FRR (Units)	PFAR (Units)	Mean/Standard Deviation/Delta (Units)	Major Actionable Events
										Component and Subsystem Ground Test(s)	Integrated Ground Test(s)
Fuel Specific Energy and Type	kWh/kg	BTU/lbm
Engine Designation and Type
Maximum Rated Thrust	kN	lbf
Maximum Rated Power	kW	hp
Core Specific Power	kW/kg	hp/lbm
Thrust Specific Fuel Consumption	g/N.s	lbm/lbf.h
Brake Specific Fuel Consumption	g/W.s	lbm/hp.h
Thrust	kN	lbf
Power	kW	hp
Speed	M	KCAS
Altitude	m	ft
Battery	SI Units	Imperial Units	At Proposal submission (Units)	SRR (Units)	PDR (Units)	CDR (Units)	FRR (Units)	PFAR (Units)	Mean/Standard Deviation/Delta (Units)	Major Actionable Events
										Component and Subsystem Ground Test(s)	Integrated Ground Test(s)
Type
Chemistry
Cell-to-System Description
C-rate and E-rate	-
Capacity	A.h
Burst Rate and Duration	- [s]
System-Level Specific Energy	Wh/kg	BTU/lbm
Cell-Level Specific Energy	Wh/kg	BTU/lbm
Operating Voltage	V (oper.)
Float Voltage	V (float)
Internal Resistance	Ω
System-level Energy Density	Wh/L	BTU/gal
Cycle Stability Criterion	cycles
Cycle Stability Criterion	cycles
Impedance Margin and Cycles	(-) [cycles]
System-level Specific Power	W/kg	hp/lbm
System-level Power Density	W/L	hp/gal
Total Thermal Management	kg/kW(th)	lbm/hp(th)
Parasitic Power	kW	hp
Safety Features Total:	kg/kW	lbm/hp
Charger Specific Power	kW/kg	hp/lbm
Charge Voltage and C-Rate	V [-]
Capacitor	SI Units	Imperial Units	At Proposal submission (Units)	SRR (Units)	PDR (Units)	CDR (Units)	FRR (Units)	PFAR (Units)	Mean/Standard Deviation/Delta (Units)	Major Actionable Events
										Component and Subsystem Ground Test(s)	Integrated Ground Test(s)
Type
Specific Energy	Wh/kg	BTU/lbm
Specific Power	W/kg	hp/lbm
Charge Voltage and Cycles	V [cycles]
Fuel Cell	SI Units	Imperial Units	At Proposal submission (Units)	SRR (Units)	PDR (Units)	CDR (Units)	FRR (Units)	PFAR (Units)	Mean/Standard Deviation/Delta (Units)	Major Actionable Events
										Component and Subsystem Ground Test(s)	Integrated Ground Test(s)
Type
Specific Power: stack-level, system-level	kW/kg	hp/lbm
Stack-to-System Description
System-level Power Density	W/L	hp/gal
Start-up Time	min.
Compressors or Pressurization System Power	kW/kg	hp/lbm
Storage	kWh/kg	BTU/lbm
Energy Carrier
Pressure	bar	psi
Safety Features Total:	kg/kW	lbm/hp
Percentage Balance of Plant	-
Total Thermal Management	kg/kW(th)	lbm/hp(th)
Parasitic Power	kW	hp
Safety Features Total:	kg/kW	lbm/hp
Motor / Generator	SI Units	Imperial Units	At Proposal submission (Units)	SRR (Units)	PDR (Units)	CDR (Units)	FRR (Units)	PFAR (Units)	Mean/Standard Deviation/Delta (Units)	Major Actionable Events
										Component and Subsystem Ground Test(s)	Integrated Ground Test(s)
Technology Notes and Approach
Maximum Power (shaft)	kW (shaft)	hp (shaft)
Maximum Power (useful)	kW (useful)	hp (useful)
Maximum Rated Motor Specific Power	kW/kg	hp/lbm
Maximum Rated Motor Specific Torque	N.m/kg	lbf.ft/lbm
Rated Motor Power	kW	hp
Rated Motor Torque	N.m	lbf.ft
Rated Motor Speed	RPM
Maximum Speed at Constant Power	RPM
Maximum Mechanical Speed	RPM
Motor Efficiency at 100% Load
Motor Efficiency at 75% Load
Motor Efficiency at 50% Load
Motor Efficiency at 25% Load
Maximum Rated Motor Linear Speed Limit	m/s	ft/s
Over-speed Limit	%RPM
Over-temperature Limits	C	F
Maximum Rated Generator Specific Power	kW/kg	hp/lbm
Rated Generator Torque	N.m	lbf.ft
Rated Generator Speed	RPM
Power Electronics Processed Power	%Rated
Total Thermal Management	kg/kW(th)	lbm/hp(th)
Parasitic Power	kW	hp
Safety Features Total:	kg/kW	lbm/hp
Propulsive Device	SI Units	Imperial Units	At Proposal submission (Units)	SRR (Units)	PDR (Units)	CDR (Units)	FRR (Units)	PFAR (Units)	Mean/Standard Deviation/Delta (Units)	Major Actionable Events
										Component and Subsystem Ground Test(s)	Integrated Ground Test(s)
Attributes of the Propulsive Device
[Ducted Fan] Pressure Ratio
Propeller/Fan Max. Corrected Tip Speed (Aero)	m/s	ft/s
Propeller/Rotor Specific Power and/or	kW/kg	hp/lbm
Fan Specific Power	kW/kg	hp/lbm
Transmission	SI Units	Imperial Units	At Proposal submission (Units)	SRR (Units)	PDR (Units)	CDR (Units)	FRR (Units)	PFAR (Units)	Mean/Standard Deviation/Delta (Units)	Major Actionable Events
										Component and Subsystem Ground Test(s)	Integrated Ground Test(s)
Gearbox Specific Power and Gearing Ratio	kW/kg (-)	hp/lbm
Total Thermal Management	kg/kW(th)	lbm/hp(th)
Parasitic Power	kW	hp
Safety Features Total:	kg/kW	lbm/hp
Power Electronics	SI Units	Imperial Units	At Proposal submission (Units)	SRR (Units)	PDR (Units)	CDR (Units)	FRR (Units)	PFAR (Units)	Mean/Standard Deviation/Delta (Units)	Major Actionable Events
										Component and Subsystem Ground Test(s)	Integrated Ground Test(s)
AC-DC Rectifier Specific Power	kW/kg	hp/lbm
Total Thermal Management	kg/kW(th)	lbm/hp(th)
Parasitic Power AC-DC	kW	hp
Safety Features Total:	kg/kW	lbm/hp
DC-AC Inverter Specific Power	kW/kg	hp/lbm
Total Thermal Management	kg/kW(th)	lbm/hp(th)
Parasitic Power DC-AC	kW	hp
Safety Features Total:	kg/kW	lbm/hp
DC-DC Converter Specific Power	kW/kg	hp/lbm
Total Thermal Management	kg/kW(th)	lbm/hp(th)
Parasitic Power DC-DC	kW	hp
Safety Features Total:	kg/kW	lbm/hp
Controller Type
Controller	kW/kg	hp/lbm
Bus Voltage for Propulsion System and Type	V [AC or DC]
Maximum Operating Power	kW	hp
Bus Voltage for Non-Prop. System And Type	V [AC or DC]
Maximum Operating Power	kW	hp
Bus AC Grid Frequency	Hz
Transmission	kg/m.kA	lbm/ft.kA
Cross-sectional Area and Wire Gauge	mm2 (-)	sq.in
EMI/EMC Shielding	kg/m.kV	lbm/ft.kV
Active Cooling Measures	kg/m.kA	lbm/ft.kA
Wiring Total Length and No. of Contactors	m (-)	ft
Protection	SI Units	Imperial Units	At Proposal submission (Units)	SRR (Units)	PDR (Units)	CDR (Units)	FRR (Units)	PFAR (Units)	Mean/Standard Deviation/Delta (Units)	Major Actionable Events
										Component and Subsystem Ground Test(s)	Integrated Ground Test(s)
Types
Specific Power	kW/kg	hp/lbm
Fault Current	A

Integrated MW-Class Powertrain

Integrated MW-Class Powertrain System Demonstration Description
Integrated MW-Class Powertrain Architectural Schematic	Demonstration Vehicle
image here	image here

Integrated MW-Class Powertrain TPMs	At Proposal submission (Units)	SRR (Units)	PDR (Units)	CDR (Units)	FRR (Units)	PFAR (Units)	Mean/Standard Deviation/Delta (Units)	Major Actionable Events - Significant series of events such as tests that may occur in between life cycle reviews and its completion triggers an assessment of TPMs as required per DRD-TE-03: Technical Data Requirements and Reporting		* Note: Please specifiy if data is (M) Measured, (D) Derived, or from a (M) Model
								Component and Subsystem Ground Test(s)	Integrated Ground Test(s)
1. Total Power level of the Integrated MW-Class Powertrain System
2. Power Level of individual electrical components
3. Operating Voltage of the Integrated MW-Class Powertrain System
4. Altitude Capability of the Integrated MW-Class Powertrain System
5. Specific Power of the Integrated MW-Class Powertrain System
6. End to End loss of the Integrated MW-Class Powertrain System
Propulsion Architecture Metrics	At Proposal submission (Units)	SRR (Units)	PDR (Units)	CDR (Units)	FRR (Units)	PFAR (Units)	Mean/Standard Deviation/Delta (Units)	Major Actionable Events
								Component and Subsystem Ground Test(s)	Integrated Ground Test(s)
Specific Power (kW/kg or hp/lbm)
Thrust Specific Power Consumption (W/N or hp/lbf)
Increment Efficiency due to Aero-propulsive (-)
Global Chain Efficiency (-)
Typical Mission Profile	Duration (min)	Length (nm)	Power Management, Allocation and Control Strategy
Stage Length
Gate
Taxi-out
Take-off
Climb
Cruise
Descent
Approach
Landing
Taxi-in
Holding/Loiter
Contingency
Diversion
Demonstration Vehicle Weights	At Proposal submission (Units)	SRR (Units)	PDR (Units)	CDR (Units)	FRR (Units)	PFAR (Units)	Mean/Standard Deviation/Delta (Units)	Major Actionable Events
								Component and Subsystem Ground Test(s)	Integrated Ground Test(s)
Maximum Take-Off Weight (kg or lbm)
Maximum Landing Weight (kg or lbm)
Manufacturer’s Weight Empty, Green (kg or lbm)
Operating Weight Empty or Basic Oper. Weight (kg or lbm)
Maximum Payload Weight (kg or lbm)
Maximum Zero-Fuel Weight (kg or lbm)
Total Release Energy Weight (kg or lbm)
Release Fuel Weight (kg or lbm)
Release Ancillary Energy Source Weight (kg or lbm)
Demonstration Vehicle Sizing Parameters and Metrics	At Proposal submission (Units)	SRR (Units)	PDR (Units)	CDR (Units)	FRR (Units)	PFAR (Units)	Mean/Standard Deviation/Delta (Units)	Major Actionable Events
								Component and Subsystem Ground Test(s)	Integrated Ground Test(s)
Wing Loading (kg/m2 or lbm/sq.ft)
Reference Wing Area (m2 or sq.ft)
Reference Wing Aspect Ratio (-)
Disc Loading (kg/m2 or lbm/sq.ft)
Reference Disc Area (m2 or sq.ft)
Number of Rotors and Number of Blades for each Rotor (-)
Maximum Mechanical Speed (RPM)
MWE / MTOW (-)
OWE (BOW) / MTOW (-)
OWE (BOW) / PAX (kg/PAX or lbm/PAX)
Release Energy Weight / MTOW (-)
MLW / MTOW (-)
Conditions Describing Total Maximum Thrust or Power
Total Maximum Thrust (kN or lbf)
Total Maximum Shaft Power (kW or hp)
All-Engines Operational Thrust-to-Weight (-)
One-Engine Inoperative Thrust-to-Weight (-)
AEO Maximum Power-to-Weight (kW/kg or hp/lbm)
AEO Maximum Power Loading (kg/kW or lbm/hp)
OEI Maximum Power-to-Weight (kW/kg or hp/lbm)
OEI Maximum Power Loading (kg/kW or lbm/hp)
Anti-torque or Tail Rotor Power (kW or hp)
Demonstration Vehicle Operational Performance	At Proposal submission (Units)	SRR (Units)	PDR (Units)	CDR (Units)	FRR (Units)	PFAR (Units)	Mean/Standard Deviation/Delta (Units)	Major Actionable Events
								Component and Subsystem Ground Test(s)	Integrated Ground Test(s)
Take-off Field Length, MTOW, ISA, SL (m or ft)
TOFL (m or ft)
Payload (kg or lbm)
Take-off Gross Weight (kg or lbm)
Specified ISA Deviation (C or F)
Specified Airport Elevation, AGL (ft)
Stall Speed and Flap Setting, MTOW, ISA, SL (KCAS)
Reference Speed and Flap Setting, MLW, ISA, SL (KCAS)
Landing Field Length, MLW ISA, SL (m or ft)
ICAO Cumulative Noise Margin to Chapter 14 (EPNdB)
ICAO NOx-Emissions Level (g/kN)
LTO NOx-Emissions (kg/LTO)
ICAO Metric Value MVCO2 (kg/km.mn)
Maximum Operating Altitude (ft)
Maximum Hover Altitude (ft)
Glide Ratio (nm/ft)
Maximum Endurance Speed (KCAS [KTAS])
Maximum Endurance Time (h)
Climb Speed Schedule (KCAS [Mach])
Maximum Rate-of-Climb, MTOW b.r., ISA, SL (fpm)
Rate-of-Climb, MTOW b.r., ISA (fpm)
Specified Altitude (ft)
Time-to-Climb to Initial Cruise Altitude (min.)
Demonstration Vehicle Max. PAX/Payload Design Range	At Proposal submission (Units)	SRR (Units)	PDR (Units)	CDR (Units)	FRR (Units)	PFAR (Units)	Mean/Standard Deviation/Delta (Units)	Major Actionable Events
								Component and Subsystem Ground Test(s)	Integrated Ground Test(s)
PAX
Range (nm)
Payload (kg or lbm)
Block Fuel (kg or lbm)
CO2-Emissions (kg or lbm)
Block Fuel per PAX (kg/PAX or lbm/PAX)
CO2-Emissions per PAX (kg/PAX or lbm/PAX)
[Fuel] Specific Air Range (nm/kg or nm/lbm)
Block Energy (MW.h or BTU)
Block Energy per PAX (MW.h/PAX or BTU/PAX)
Degree-of-Hybridization for Block Energy (-)
Energy Specific Air Range (nm/kW.h or nm/BTU)
Miss. Energy Index (kW.h/kg.nm or BTU/lbm.nm)
Demonstration Vehicle Max. PAX/Payload Off-Design Stage Length	At Proposal submission (Units)	SRR (Units)	PDR (Units)	CDR (Units)	FRR (Units)	PFAR (Units)	Mean/Standard Deviation/Delta (Units)	Major Actionable Events
								Component and Subsystem Ground Test(s)	Integrated Ground Test(s)
PAX
Stage Length (nm)
Payload (kg or lbm)
Block Fuel (kg or lbm)
CO2-Emissions (kg or lbm)
Block Fuel per PAX (kg/PAX or lbm/PAX)
CO2-Emissions per PAX (kg/PAX or lbm/PAX)
[Fuel] Specific Air Range (nm/kg or nm/lbm)
Block Energy (MW.h or BTU)
Block Energy per PAX (MW.h/PAX or BTU/PAX)
Degree-of-Hybridization for Block Energy (-)
Energy Specific Air Range (nm/kW.h or nm/BTU)
Miss. Energy Index (kW.h/kg.nm or BTU/lbm.nm)
Integrated MW-Class Powertrain Components and Subsystems
Engine	SI Units	Imperial Units	At Proposal submission (Units)	SRR (Units)	PDR (Units)	CDR (Units)	FRR (Units)	PFAR (Units)	Mean/Standard Deviation/Delta (Units)	Major Actionable Events
										Component and Subsystem Ground Test(s)	Integrated Ground Test(s)
Fuel Specific Energy and Type	kWh/kg	BTU/lbm
Engine Designation and Type
Maximum Rated Thrust	kN	lbf
Maximum Rated Power	kW	hp
Core Specific Power	kW/kg	hp/lbm
Thrust Specific Fuel Consumption	g/N.s	lbm/lbf.h
Brake Specific Fuel Consumption	g/W.s	lbm/hp.h
Thrust	kN	lbf
Power	kW	hp
Speed	M	KCAS
Altitude	m	ft
Battery	SI Units	Imperial Units	At Proposal submission (Units)	SRR (Units)	PDR (Units)	CDR (Units)	FRR (Units)	PFAR (Units)	Mean/Standard Deviation/Delta (Units)	Major Actionable Events
										Component and Subsystem Ground Test(s)	Integrated Ground Test(s)
Type
Chemistry
Cell-to-System Description
C-rate and E-rate	-
Capacity	A.h
Burst Rate and Duration	- [s]
System-Level Specific Energy	Wh/kg	BTU/lbm
Cell-Level Specific Energy	Wh/kg	BTU/lbm
Operating Voltage	V (oper.)
Float Voltage	V (float)
Internal Resistance	Ω
System-level Energy Density	Wh/L	BTU/gal
Cycle Stability Criterion	cycles
Cycle Stability Criterion	cycles
Impedance Margin and Cycles	(-) [cycles]
System-level Specific Power	W/kg	hp/lbm
System-level Power Density	W/L	hp/gal
Total Thermal Management	kg/kW(th)	lbm/hp(th)
Parasitic Power	kW	hp
Safety Features Total:	kg/kW	lbm/hp
Charger Specific Power	kW/kg	hp/lbm
Charge Voltage and C-Rate	V [-]
Capacitor	SI Units	Imperial Units	At Proposal submission (Units)	SRR (Units)	PDR (Units)	CDR (Units)	FRR (Units)	PFAR (Units)	Mean/Standard Deviation/Delta (Units)	Major Actionable Events
										Component and Subsystem Ground Test(s)	Integrated Ground Test(s)
Type
Specific Energy	Wh/kg	BTU/lbm
Specific Power	W/kg	hp/lbm
Charge Voltage and Cycles	V [cycles]
Fuel Cell	SI Units	Imperial Units	At Proposal submission (Units)	SRR (Units)	PDR (Units)	CDR (Units)	FRR (Units)	PFAR (Units)	Mean/Standard Deviation/Delta (Units)	Major Actionable Events
										Component and Subsystem Ground Test(s)	Integrated Ground Test(s)
Type
Specific Power: stack-level, system-level	kW/kg	hp/lbm
Stack-to-System Description
System-level Power Density	W/L	hp/gal
Start-up Time	min.
Compressors or Pressurization System Power	kW/kg	hp/lbm
Storage	kWh/kg	BTU/lbm
Energy Carrier
Pressure	bar	psi
Safety Features Total:	kg/kW	lbm/hp
Percentage Balance of Plant	-
Total Thermal Management	kg/kW(th)	lbm/hp(th)
Parasitic Power	kW	hp
Safety Features Total:	kg/kW	lbm/hp
Motor / Generator	SI Units	Imperial Units	At Proposal submission (Units)	SRR (Units)	PDR (Units)	CDR (Units)	FRR (Units)	PFAR (Units)	Mean/Standard Deviation/Delta (Units)	Major Actionable Events
										Component and Subsystem Ground Test(s)	Integrated Ground Test(s)
Technology Notes and Approach
Maximum Power (shaft)	kW (shaft)	hp (shaft)
Maximum Power (useful)	kW (useful)	hp (useful)
Maximum Rated Motor Specific Power	kW/kg	hp/lbm
Maximum Rated Motor Specific Torque	N.m/kg	lbf.ft/lbm
Rated Motor Power	kW	hp
Rated Motor Torque	N.m	lbf.ft
Rated Motor Speed	RPM
Maximum Speed at Constant Power	RPM
Maximum Mechanical Speed	RPM
Motor Efficiency at 100% Load
Motor Efficiency at 75% Load
Motor Efficiency at 50% Load
Motor Efficiency at 25% Load
Maximum Rated Motor Linear Speed Limit	m/s	ft/s
Over-speed Limit	%RPM
Over-temperature Limits	C	F
Maximum Rated Generator Specific Power	kW/kg	hp/lbm
Rated Generator Torque	N.m	lbf.ft
Rated Generator Speed	RPM
Power Electronics Processed Power	%Rated
Total Thermal Management	kg/kW(th)	lbm/hp(th)
Parasitic Power	kW	hp
Safety Features Total:	kg/kW	lbm/hp
Propulsive Device	SI Units	Imperial Units	At Proposal submission (Units)	SRR (Units)	PDR (Units)	CDR (Units)	FRR (Units)	PFAR (Units)	Mean/Standard Deviation/Delta (Units)	Major Actionable Events
										Component and Subsystem Ground Test(s)	Integrated Ground Test(s)
Attributes of the Propulsive Device
[Ducted Fan] Pressure Ratio
Propeller/Fan Max. Corrected Tip Speed (Aero)	m/s	ft/s
Propeller/Rotor Specific Power and/or	kW/kg	hp/lbm
Fan Specific Power	kW/kg	hp/lbm
Transmission	SI Units	Imperial Units	At Proposal submission (Units)	SRR (Units)	PDR (Units)	CDR (Units)	FRR (Units)	PFAR (Units)	Mean/Standard Deviation/Delta (Units)	Major Actionable Events
										Component and Subsystem Ground Test(s)	Integrated Ground Test(s)
Gearbox Specific Power and Gearing Ratio	kW/kg (-)	hp/lbm
Total Thermal Management	kg/kW(th)	lbm/hp(th)
Parasitic Power	kW	hp
Safety Features Total:	kg/kW	lbm/hp
Power Electronics	SI Units	Imperial Units	At Proposal submission (Units)	SRR (Units)	PDR (Units)	CDR (Units)	FRR (Units)	PFAR (Units)	Mean/Standard Deviation/Delta (Units)	Major Actionable Events
										Component and Subsystem Ground Test(s)	Integrated Ground Test(s)
AC-DC Rectifier Specific Power	kW/kg	hp/lbm
Total Thermal Management	kg/kW(th)	lbm/hp(th)
Parasitic Power AC-DC	kW	hp
Safety Features Total:	kg/kW	lbm/hp
DC-AC Inverter Specific Power	kW/kg	hp/lbm
Total Thermal Management	kg/kW(th)	lbm/hp(th)
Parasitic Power DC-AC	kW	hp
Safety Features Total:	kg/kW	lbm/hp
DC-DC Converter Specific Power	kW/kg	hp/lbm
Total Thermal Management	kg/kW(th)	lbm/hp(th)
Parasitic Power DC-DC	kW	hp
Safety Features Total:	kg/kW	lbm/hp
Controller Type
Controller	kW/kg	hp/lbm
Bus Voltage for Propulsion System and Type	V [AC or DC]
Maximum Operating Power	kW	hp
Bus Voltage for Non-Prop. System And Type	V [AC or DC]
Maximum Operating Power	kW	hp
Bus AC Grid Frequency	Hz
Transmission	kg/m.kA	lbm/ft.kA
Cross-sectional Area and Wire Gauge	mm2 (-)	sq.in
EMI/EMC Shielding	kg/m.kV	lbm/ft.kV
Active Cooling Measures	kg/m.kA	lbm/ft.kA
Wiring Total Length and No. of Contactors	m (-)	ft
Protection	SI Units	Imperial Units	At Proposal submission (Units)	SRR (Units)	PDR (Units)	CDR (Units)	FRR (Units)	PFAR (Units)	Mean/Standard Deviation/Delta (Units)	Major Actionable Events
										Component and Subsystem Ground Test(s)	Integrated Ground Test(s)
Types
Specific Power	kW/kg	hp/lbm
Fault Current	A

File details come from the government source that posted it. Updated Apr 9, 2021.