engine technical questionnaire specification …...engine technical questionnaire specification...

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Engine Technical Questionnaire Specification Worksheet PLATFORM TECHNICAL SPECIFICATION UNIT OF CUSTOMER RESPONSE MEASURE 1 Anticipated maximum takeoff weight? 2 Anticipated maximum required endurance? Hours 3 Max. weight of all up propulsion system, including prop, harnesses and cowlings. If fuel tanks and delivery system are being supplied, provide max. weight of the PMU with fuel/oil tanks filled and system primed. 4 Maximum estimated weight of engine – core only 5 Power required over minutes? 6 Target time between overhauls (TBO) for engine? Hours 7 Fuel Specification? 8 Oil Specification? 9 Anticipated general mission profile? RPM/hp (e.g. max. peak - takeoff; max continuous - est. 3 hrs; cruise/loiter - est. 5 hrs; max continuous - est. 3 hrs; landing/mission end.) 10 Variable pitch propeller system? Blades Number of Blades Number 11 Direction of propeller rotation from back of aircraft, looking forward? 12 Aircraft Engine Configuration Type? 13 Is generator required? (Interface data/drawings of generator, required.) If Yes: Required power/generator? kW 14 Does system require in-flight starting? 15 G-Load at launch? g G-Load at capture? g 16 Number of platforms/units required for testing? Number 17 Expected volume per year over years? Number 18 Is system currently in a program? If Yes: Number of units currently in service? Number 19 Expected development program outline and time line? (e.g. TBO test of engine required? Flight test period? Flight test platform expected same as production?) DATE SUBMITTED Company Name Name Email Phone Mobile Project Platform/ Program Regulation & Specification Regulation & Specification NWUAV will not share nor export any information here- in without first obtaining the appropriate governmental approvals. All information provided shall remain confidential F-720-005 REV 4 Property of Northwest UAV Propulsion Systems Approved by: J. Kendall 11/8/2016 Northwest UAV Propulsion Systems 11160 SW Durham Lane, Suite 1 | McMinnville, OR 97128 Office: 503.434.6845 | Fax: 503.217.1917 | www.nwuav.com Information, questions and form submission: [email protected] or call 1-503-434-6845

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Page 1: Engine Technical Questionnaire Specification …...Engine Technical Questionnaire Specification Worksheet Platform/ Program Information or Questions Please Contact: Joe Gibbs, VP Business

Engine Technical QuestionnaireSpecification Worksheet

PLATFORM TECHNICAL SPECIFICATION UNIT OF CUSTOMER RESPONSE MEASURE

1 Anticipated maximum takeoff weight?

2 Anticipated maximum required endurance? Hours

3

Max. weight of all up propulsion system, including prop, harnesses and cowlings. If fuel tanks and delivery system are being supplied, provide max. weightofthePMUwithfuel/oiltanksfilledandsystemprimed.

4 Maximum estimated weight of engine – core only

5 Power required over minutes?

6 Target time between overhauls (TBO) for engine? Hours

7 FuelSpecification?

8 OilSpecification?

9 Anticipatedgeneralmissionprofile?

RPM/hp (e.g. max. peak - takeoff; max continuous - est. 3 hrs; cruise/loiter - est. 5 hrs; max continuous - est. 3 hrs; landing/mission end.)

10

Variable pitch propeller system?

Blades Number of Blades Number

11 Direction of propeller rotation from back of aircraft, looking forward?

12 AircraftEngineConfigurationType?

13

Is generator required? (Interface data/drawings of generator, required.) If Yes: Required power/generator? kW

14 Doessystemrequirein-flightstarting?

15

G-Load at launch? g G-Load at capture? g

16 Number of platforms/units required for testing? Number

17 Expected volume per year over years? Number

18

Is system currently in a program?

If Yes: Number of units currently in service? Number

19

Expected development program outline and time line? (e.g. TBO test of engine required? Flight test period? Flight test platform expected same as production?)

DATE SUBMITTED

CONTACT INFORMATION

Company Name

Name Email

Phone Mobile

Project

Platform/Program

Regulation & SpecificationRegulation & Specification

NWUAV will not share nor export any information here-in without first obtaining the appropriate governmental approvals.Allinformationprovidedshallremainconfidential

F-720-005 REV 4Property of Northwest UAV Propulsion Systems Approved by: J. Kendall 11/8/2016

Northwest UAV Propulsion Systems11160 SW Durham Lane, Suite 1 | McMinnville, OR 97128Office:503.434.6845|Fax:503.217.1917|www.nwuav.com

Information, questions and form submission: [email protected]

or call 1-503-434-6845