AIR FORCE MIL-STD-3013 A-2008 GLOSSARY OF DEFINITIONS GROUND RULES AND MISSION PROFILES TO DEFINE AIR VEHICLE PERFORMANCE CAPABILITY《航空器性能水平界定用定义 基本法则和任务概述用词汇》.pdf

《AIR FORCE MIL-STD-3013 A-2008 GLOSSARY OF DEFINITIONS GROUND RULES AND MISSION PROFILES TO DEFINE AIR VEHICLE PERFORMANCE CAPABILITY《航空器性能水平界定用定义 基本法则和任务概述用词汇》.pdf》由会员分享，可在线阅读，更多相关《AIR FORCE MIL-STD-3013 A-2008 GLOSSARY OF DEFINITIONS GROUND RULES AND MISSION PROFILES TO DEFINE AIR VEHICLE PERFORMANCE CAPABILITY《航空器性能水平界定用定义 基本法则和任务概述用词汇》.pdf（131页珍藏版）》请在麦多课文档分享上搜索。

1、 MIL-STD-3013A 9 September 2008 SUPERSEDING MIL-STD-3013 14 February 2003 DEPARTMENT OF DEFENSE STANDARD PRACTICE GLOSSARY OF DEFINITIONS, GROUND RULES, AND MISSION PROFILES TO DEFINE AIR VEHICLE PERFORMANCE CAPABILITY AMSC N/A FSC 15GP DISTRIBUTION STATEMENT A. Approved for public release; distribu

2、tion is unlimited. INCH-POUND Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-STD-3013A ii FOREWORD 1. This standard is approved for use by all Departments and Agencies of the Department of Defense. 2. Microsoft Word and Adobe Acrobat versions of

3、 this document contain hyperlinks which are identifiable by blue-font characters. Once selected, a hyperlink will take the user to a referenced paragraph, table, figure, and Website. The simplest way to return to the place of origin within a Microsoft Word document is to click the back arrow on the

4、Web toolbar. This toolbar can be displayed by selecting View and Toolbars on the menu bar, and then selecting the Web option. This same method can be employed in Adobe Acrobat versions of a document: select View and Toolbars on the menu bar, and then select Navigation. The back arrow and forward arr

5、ow allow the user to return to the place of origin after a hyperlink has been selected. 3. Comments, suggestions, or questions on this document should be addressed to ASC/ENRS, 2530 Loop Road West, Wright-Patterson AFB OH 45433-7101; or e-mailed to Engineering.Standardswpafb.af.mil. Since contact in

6、formation can change, you may want to verify the currency of this address information using the ASSIST Online database at http:/assist.daps.dla.mil. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-STD-3013A iii CONTENTS PARAGRAPH PAGE 1. SCOPE 1

7、1.1 Purpose 1 1.2 Applicability . 1 1.3 Application guidance 1 2. APPLICABLE DOCUMENTS . 1 2.1 General 1 2.2 Government documents 1 2.2.1 Specifications, standards, and handbooks . 1 2.2.2 Other Government documents, drawings, and publications 2 2.3 Non-Government publications 2 2.4 Order of precede

8、nce 2 3. DEFINITIONS 3 3.1 Missions 8 3.1.1 Range 8 3.1.2 Radius . 8 3.1.3 Mission Types . 8 3.1.3.2 Clean Mission . 8 3.1.3.3 Ferry Mission 8 3.1.3.3.1 Alternate Design Criteria 8 3.1.3.4 Inflight Refueled Mission . 8 3.1.3.4.1 Rendezvous Refuel . 8 3.1.3.4.2 Buddy Refuel 8 3.1.4 Mission Categories

9、 8 3.1.4.1 Combat Air Patrol (CAP) 8 3.1.4.2 Close Air Support (CAS) 8 3.1.4.3 Suppression of Enemy Air Defenses (SEAD) . 9 3.1.4.4 Interdiction 9 3.1.4.5 Intercept 9 3.1.4.6 Cargo/Troop Transport . 9 3.1.4.7 Observation/Reconnaissance. 9 3.1.4.8 Anti-Submarine/Anti-Surface Warfare (ASW/ASUW) 9 3.1.

10、4.9 Bomber 9 3.1.4.10 Trainer . 9 3.1.4.11 Airborne Warning and Control . 9 3.1.5 Times 9 3.1.5.1 Mission Time 9 3.1.5.2 Cycle Time 9 3.1.5.3 Block Time 9 3.1.5.4 Intercept Time . 9 3.2 Takeoff 9 3.2.1 Rotation Speed (Vrot) . 10 3.2.3.1.1 Alternate Design Criteria 10 3.2.2 Stall Speed (Vs) 10 3.2.2.

11、1 Power-Off Stall Speed (Vspo) 10 3.2.2.2 Power-On Stall Speed (Vsp) . 10 3.2.3 Liftoff Speed (Vlo) 11 3.2.3.1 Land Operations 11 3.2.3.1.1 Alternate Design Criteria 11 3.2.3.2 Carrier Operations . 11 3.2.3.2.1 Catapult Minimum End Airspeed (Vc) . 11 3.2.3.2.1.1 Computational Ground Rules 11 3.2.3.2

12、.2 Minimum Wind-Over-Deck (WOD) (Catapult) 12 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-STD-3013A iv CONTENTS - Continued PARAGRAPH PAGE 3.2.3.2.2.1 Operational Wind-Over-Deck (WOD) (Catapult) . 12 3.2.3.2.3 Catapult Operational End Airspee

13、d (Vop) 12 3.2.3.2.3.1 Catapult Endspeed Including Thrust Effects (VA) . 12 3.2.3.2.4 STOVLV/STOL air vehicle 13 3.2.3.2.4.1 STOVL Minimum Flight Speed (Vmin(STOVL) . 13 3.2.3.2.4.1 Deck Minimum End Airspeed (short Takeoff) (Vend(m) . 13 3.2.3.2.4.1.2 Computational Ground Rules 13 3.2.3.2.4.3 Minimu

14、m Wind-Over-Deck (Short Takeoff) . 13 3.2.3.2.4.3.1 Operational Wind-Over-Deck (Short Takeoff) . 13 3.2.3.2.4.4 Deck Endspeed (Vend) 14 3.2.3.2.4.4.1 Deck Operational End Airspeed (Vend(op) 14 3.2.3.3 STOVL Short Takeoff 14 3.2.3.3.1 Operational Wind Over Deck (Short Takeoff) 14 3.2.3.3.1.1 Minimum

15、Wind Over Deck (Short Takeoff) (WOD). 14 3.2.3.3.2 Deck Endspeed (Short Takeoff) (Vend) 14 3.2.3.3.2.1 Deck Operational End Airspeed (Vend(op) . 14 3.2.3.3.3 STOVL Flat Deck Short Takeoff 14 3.2.3.3.3.1 Deck Minimum End Airspeed (Short Takeoff) (Vend(m) . 14 3.2.3.3.3.2 Ship-based Flat Deck Short Ta

16、keoff Distance 14 3.2.3.3.3.2.1 Computational Ground Rules 14 3.2.3.3.4 STOVL Ski Jump Short Takeoff . 15 3.2.3.3.4.1 Deck Minimum End Airspeed (Short Takeoff) (Vend(m) . 15 3.2.3.3.4.2 Ship-based Ski Jump Short Takeoff Distance . 15 3.2.3.3.4.2.1 Computational Ground Rules 15 3.2.3.4 Austere Site O

17、perations 15 3.2.3.4.1 STOVL Short Takeoff Speed 15 3.2.3.4.2 Land-based Short Takeoff Distance 16 3.2.3.4.2.1 Computational Ground Rules 16 3.2.3.4.3 STOVL Vertical Takeoff 16 3.2.3.4.3.1 Computational Ground Rules 16 3.2.4 Obstacle Clearance Speed (Vobs) . 17 3.2.4.1 Alternate Design Criteria 17 3

18、.2.5 Ground Minimum Control Speed (Vmcg) 17 3.2.6 Air Minimum Control Speed (Vmca) 17 3.2.6.1 Static Air Minimum Control Speed (Vmcas) 17 3.2.6.2 Dynamic Air Minimum Control Speed (Vmcad) 17 3.2.7 Ground Run Distance 17 3.2.7.1 Alternate Design Criteria 18 3.2.8 Total Takeoff Distance 18 3.2.9 Groun

19、d Effect 18 3.2.9.1 Out-of-Ground Effect (OGE) 18 3.2.9.2 In-Ground Effect (IGE) . 18 3.2.9.2.1 In-Ground Effect (V/STOL air vehicles) 19 3.2.10 Critical Field Length (CFL) 19 3.2.10.1 Computational Ground Rules 20 3.2.10.2 Alternate Design Criteria 20 3.2.11 Critical Engine Failure Speed (Vcef) 21

20、3.2.13 Refusal Distance . 21 3.2.14 Coefficient of Friction ( ) . 21 3.2.14.1 Alternate Design Criteria 21 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-STD-3013A v CONTENTS - Continued PARAGRAPH PAGE 3.3 Climb 22 3.3.1 Rate-of-Climb (R/C) . 22

21、 3.3.1.1 Maximum Rate-of-Climb 22 3.3.1.2 Dynamic Rate-of-Climb 22 3.3.1.4 Engine Out Rate-Of-Climb . 23 3.3.1.4.1 Alternate Design Criteria (Carrier) . 23 3.3.2 Climb Gradient 24 3.3.3 Flight Path Angle ( ) . 24 3.3.4 Initial Climb-Out . 24 3.3.5 Enroute Climb . 24 3.3.5.1 Minimum Time to Climb 24

22、3.3.5.2 Minimum Fuel to Climb . 24 3.3.6 Recovery Climb 24 3.3.7 Zoom Climb 24 3.3.8 ombat Climb 24 3.3.9 Climb Speed 24 3.3.9.1 Climb Schedule . 24 3.3.9.2 Best Climb Speed 24 3.3.9.3 Optimum Climb Speed 24 3.4 Ceiling . 24 3.4.1 Absolute Ceiling . 24 3.4.2 Service Ceiling 25 3.4.3 Cruise Ceiling .

23、 25 3.4.4 Combat Ceiling . 25 3.5 Cruise 25 3.5.1 Cruise Altitude 25 3.5.2 Optimum Cruise Speed/Altitude . 25 3.5.3 Constant Altitude Cruise . 25 3.5.4 Cruise Climb . 25 3.5.5 Step Climb Cruise . 25 3.5.6 Maximum-Range Cruise Speed 25 3.5.7 Long-Range Cruise Speed 25 3.5.8 Average Cruise Speed . 25

24、3.5.9 Maximum Cruise Speed 25 3.5.10 Specific Range (SR) 26 3.5.11 Range Factor (RF) . 26 3.5.12 Cruise Figure of Merit (FM) . 26 3.5.13 Combat Altitude 26 3.5.14 Penetration Speed 26 3.5.15 Withdrawal Speed . 26 3.5.16 Maximum Speed . 27 3.5.16.1 Level Flight Maximum Speed (VH) . 27 3.5.16.2 Limit

25、Speed (VL) 27 3.5.16.3 Dive Speed (VD) . 27 3.6 Endurance . 27 3.6.1 Maximum Endurance Speed . 27 3.6.2 Maximum Endurance Altitude 27 3.6.3 Combat Loiter Speed 27 3.6.3.1 Alternate Design Criteria 27 3.7 Descent 27 3.7.1 Rate-of-Descent (R/D) 27 3.7.2 Descent Speed . 28 Provided by IHSNot for Resale

26、No reproduction or networking permitted without license from IHS-,-,-MIL-STD-3013A vi CONTENTS - Continued PARAGRAPH PAGE 3.7.3 Enroute Descent 28 3.7.4 Maximum Range Descent . 28 3.7.5 Penetration Descent. 28 3.7.6 Emergency (Minimum Time) Descent 28 3.7.7 Alternate Design Criteria 28 3.8 Landing .

27、 28 3.8.1 Approach Speed (Vpa) 29 3.8.1.1 Land-Based Air Vehicles 29 3.8.1.1.1 Alternate Design Criteria 29 3.8.1.2 Carrier-Based Air Vehicles . 29 3.8.2 Touchdown Speed . 30 3.8.2.1 Land Operations (Vtdl) . 30 3.8.2.1.1 Alternate Design Criteria 30 3.8.2.2 Carrier Operations (Vtdc) 30 3.8.2.2.1 Win

28、d-Over-Deck (Landing) 30 3.8.2.2.2 Waveoff. 30 3.8.2.2.2.1 Computational Ground Rules 31 3.8.2.2.3 Shipboard Engaging Speed (Ve) . 31 3.8.2.2.4 Bolter 31 3.8.2.2.4.1 Computational Ground Rules 32 3.8.2.2.4.1.1 Alternate Design Criteria 32 3.8.3 Ground Roll Distance 32 3.8.4 Landing Air Run Distance

29、32 3.8.5 Total Landing Distance . 32 3.8.5.1 Alternate Design Criteria 32 3.8.5.1.1 Short Field Landing Distance 33 3.8.6 Maximum Brake Energy Speed 33 3.8.7 Maximum Vertical Landing Weight (V/STOL Air Vehicles) 33 3.8.7.1 Thrust (Power) Margin - Control and Stationkeeping (V/STOL Air Vehicles) . 33

30、 3.8.8 STOVL Vertical Mode Operations . 34 3.8.8.1 Control Power for Vertical Operations . 34 3.8.8.2 Vertical Landing (VL) 34 3.8.8.2.1 Computational Ground Rules 34 3.8.8.2.2 Lift Budget Description 34 3.8.8.2.3 In-Ground Effect Vertical Landing Waveoff 35 3.8.8.2.3.1 In-Ground Effect Vertical Lan

31、ding Waveoff Weight . 35 3.8.8.3 Short Landing 35 3.8.8.3.1 Short Landing Touchdown Speed . 35 3.8.8.3.1.1 STOVL Minimum Flight Speed 35 3.8.8.3.2 Short Landing Distance . 35 3.8.8.3.2.1 Computational Ground Rules 35 3.8.8.4 Rolling Vertical Landing 36 3.9 Maneuver 36 3.9.1 Flight Envelope . 36 3.9.

32、2 Load Factor . 36 3.9.2.1 Normal Load Factor (body axis) (nz) 36 3.9.2.2 Normal Load Factor (wind axis) (nl) 36 3.9.2.2.1 Sustained Load Factor . 36 3.9.2.2.2 Instantaneous Load Factor 36 3.9.3 Specific Excess Power (Ps) . 37 3.9.4 Specific Energy (Es) . 37 Provided by IHSNot for ResaleNo reproduct

33、ion or networking permitted without license from IHS-,-,-MIL-STD-3013A vii CONTENTS - Continued PARAGRAPH PAGE 3.9.5 Energy Exchange ( E) 37 3.9.6 Combat Speed . 37 3.9.7 Corner Speed . 37 3.9.7.1 Sustained Corner Speed 37 3.9.7.2 Instantaneous Corner Speed 37 3.10 Weights . 38 3.10.1 Weight Empty .

34、 38 3.10.2 Basic Weight . 38 3.10.3 Operating Weight 38 3.10.4 Payload 38 3.10.5 Flight Design Gross Weight 38 3.10.6 Maximum Ground Weight 38 3.10.7 Maximum Flight Weight . 38 3.10.8 Takeoff Gross Weight . 39 3.10.9 Maximum Takeoff Gross Weight . 39 3.10.10 Mission Landing Weight . 39 3.10.11 Maxim

35、um Landing Weight . 39 3.10.12 Combat weight 39 3.10.12.2 Nonmission-Based Combat Weight 40 3.10.13 Carrier Bringback Weight . 40 3.10.13.1 Vertical Landing Bringback Weight (STOVL) . 40 3.10.14 Weight definition guide 41 3.10.15 Maximum Catapult Design Gross Weight 42 3.10.16 Maximum Catapult Weigh

36、t . 42 3.10.17 Primary Catapult Mission Weight . 42 3.10.18 Landplane Landing Weight . 42 3.10.19 Maximum Landing Weight . 42 3.10.20 Carrier Landing Design Gross Weight 42 3.10.21 Barricade Design Gross Weight 42 3.10.22 Vertical Landing Design Gross Weight (STOVL) 42 3.10.23 Maximum Landing Gear J

37、acking Weight . 42 3.10.24 Maximum Airframe Jacking Weight. 42 3.10.25 Hoisting Weight 42 3.11 Propulsion . 42 3.11.1 Engine Performance Level 42 3.11.1.1 Engine Performance-Level Definitions . 42 3.11.1.1.1 Specification Performance 42 3.11.1.1.2 Minimum Performance . 43 3.11.1.1.3 Status Performan

38、ce . 43 3.11.1.2 Engine Performance-Level Use Guidelines 43 3.11.1.2.1 Lead-the-Fleet . 44 3.11.1.2.2 Endurance Testing. 44 3.11.2 Engine Service Time Definitions 44 3.11.2.1 New Engine . 44 3.11.2.2 Deteriorated Engine 44 3.11.3 Engine Power Setting Definitions . 44 3.11.3.1 Idle Thrust (Power) . 4

39、4 3.11.3.2 Engine Type-Specific Power Settings . 44 3.11.3.2.1 Shaft Power Engines . 44 3.11.3.2.2 Nonaugmented Jet Engines . 45 3.11.3.2.3 Augmented Jet Engines . 45 3.12 Fuel . 46 3.12.1 Alternate Design Criteria 46 Provided by IHSNot for ResaleNo reproduction or networking permitted without licen

40、se from IHS-,-,-MIL-STD-3013A viii CONTENTS - Continued PARAGRAPH PAGE 3.13 Surface Damage Criteria . 46 3.13.1 STOVL Operations Surface Compatibility . 46 4. GENERAL REQUIREMENTS 49 4.1 Computational Ground Rules 49 4.1.1 Speeds . 49 4.1.2 Atmosphere . 49 4.1.2.1 Alternate Design Criteria 49 4.1.3

41、Wind 49 4.1.4 Formation Flight . 49 4.1.5 Ordnance Expenditure . 49 4.1.6 External Fuel Tanks 49 4.1.7 Pylons/Racks . 49 4.1.8 Change in Energy State at Intersection of Mission Segments . 49 4.1.9 Reduced Engine Operation . 49 4.1.10 Authorized Operation 49 4.1.11 Trainer Air Vehicles 50 4.1.12 Vari

42、able Geometry Wing Air Vehicles . 50 4.1.13 Fuel Consumption Tolerance 50 4.1.14 Fuel Consumption Corrections . 50 4.2 Mission Segment Ground Rules 50 4.2.1 Warm-up and Takeoff . 50 4.2.2 Climb 52 4.2.2.1 Initial Climb-Out . 52 4.2.2.1.1 All Engines Operating (AEO) . 52 4.2.2.1.2 One Engine Inoperat

43、ive (OEI) 52 4.2.2.2 Enroute Climb . 52 4.2.2.2.1 Enroute Climb Data 52 4.2.2.2.2 Enroute Climb Power 52 4.2.3 Cruise 52 4.2.4 Penetration and Withdrawal 52 4.2.5 Combat 53 4.2.6 Loiter . 53 4.2.6.1 Mission-Specific Tasks . 53 4.2.7 Refueling . 54 4.2.7.1 Rendezvous Refuel . 54 4.2.7.2 Buddy Refuel

44、54 4.2.8 Descent 54 4.2.9 Landing Reserves 55 4.2.9.1 Land Operations 55 4.2.9.2 Carrier Operation 56 4.2.9.2.1 Visual Flight Rules (VFR) 56 4.2.9.2.2 Instrument Flight Rules (IFR) . 57 4.2.9.2.3 100 Nautical Mile BINGO 57 4.2.9.2.4 Other . 58 4.2.9.3 Vertical Landing . 58 5. DETAILED REQUIREMENTS .

45、 59 6. NOTES 60 6.1 Intended use 60 6.2 Acquisition requirements 60 6.3 Subject term (key word) listing . 60 6.4 Changes from previous issue 60 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-STD-3013A ix CONTENTS - Continued PAGE TABLES TABLE I.

46、 Symbols and abbreviations . 5 TABLE II. Coefficient of friction 21 TABLE III. Engine performance levels 43 TABLE IV. Non-afterburning thrust (power) settings 45 TABLE V. Fuel consumption 55 FIGURES FIGURE 1. Air vehicle force balance diagram 4 FIGURE 2. Takeoff terminology . 10 FIGURE 3. Ground eff

47、ects . 19 FIGURE 4. Critical field length terminology . 19 FIGURE 5. Critical field length criteria . 20 FIGURE 6. Landing terminology . 28 FIGURE 7. Lift budget example 34 FIGURE 8. Energy manuever diagram 38 FIGURE 9. Runway grade concrete time to damage as a function of jet conditions . 46 FIGURE

48、 10. AM-2 mat time to damage as a function of jet conditions 47 FIGURE 11. Ship deck non-skid (MS-440G) time to damage as a function of jet conditions . 47 FIGURE 12. Road grade asphalt time to damage as a function of jet conditions 48 FIGURE 13. Fuel for flight to an alternate field 56 Provided by IHSNot for Re