1、MILP-22203 (Aer j 21 September 1959 MILITARY SPECIFICATION PERFORMANCE DATA REPORT FOR STANDARD AIRCRAFT CHARACTERISTICS CHARTS FOR PILOTED AIRCRAFT This specification has been approved by the Bureau of Aeronautics , Department of the Navy TABLE OF COhlEKTS SCOPE Scope Application Classification APP
2、LICABLE SPECIFICATIONS AND OPHER PWLICATIONS Specifications REQIREMETiS General Requirements Basic Data Perforn?ance Data Report Text Introduction Tabulated Data Aerodynamic Data Thrust Required Thrust Available Perf mmance Carrier Suitability In-Flight Refueling Reference Material Missions QUALITY
3、ASSWCE PROVISIONS Inspection and Acceptance PREPARATION FOR DELIVERY Packing Marking and Labeling Interpretation NOTES 1- ParagraDh 1 1.1 1.2 1.3 . 2 2.1 3 3.1 3.1.1 3.1.2.1 3.1.2.1.2 3.1.2.1.4 3.1.2.1.6 3 -1.2 3.1.2.1.1 3.1.2.1.3 3.1.2.1.5 3.1.2,1.7 3.1.2.1.8 3.1.2.1.9 3 e2 4 4.1 5 5.1 5 e2 5.2.1 6
4、 6.1 i - I .P c Licensed by Information Handling ServicesMIL-P-22203 TM 399990b 0225273 T m- 1 MILP22203(Aer) 1. SCOPE 1.1 , the substantiating Performance Data Report for the Standard Aircraft Characteristics (SA3 charts required by Specification MILD-8706 (Aer) and by addenda thereto. distributed
5、throughout, the Department of Defense and to other interested agencies, are the official means of delineating the performance of naval aircraft, and as such must contain accurate and realistic information. The Performance Dta Report, substantiating the information given in the Standard Aircraft Char
6、acteristics charts must be sufficienkly complete to expedite a prompt investigation and review of the derk.ed performance and to permit additional calculations to be made by personnel of the Bureau of Aeronautics as required. 1.2 APPLICATION.- The characteristics charts and reports described herein
7、are based on the Standard Aircraft Characteristic8 charts governed by the coordinated Specification MILD-50118. for piloted aircraft. This specification details that portion of MIM-501U which governs the submittal of the substantiating Performance Data Reports and pertinent graphs associated with th
8、ese reports. 1.3 is prohibited. SCOPE.-This specification governs the definitions of the requirements for, and methods of presenti The Standard Aircraft Characteristics charts, which are CLASSIFICATION.- Performance DataReports are to be presented in the mer prescribed in this specification. Unautho
9、rized reproduction of such reports 2. APPLICABLE SIFICATIONS AND CIPHER PWLICATIONS 2.1 This specification implements, amplifies, or invokes the following pub- lications, of latest issue date in effect. SPECIFIC AT IONS biL1TAR.Y MIL-C-501lA Charts; Standard Aircraft Characteristics and Performance,
10、Piloted MIL-D-8706(Aer) Data, Design; Contract Requirements for Aircraft MIL-D-7822 Drawings; For Standard Aircraft Characteristics and Performanbe charts, (When requesting specifications, standards, drawinge, and publications refer to both title and number. upon application to the Commanding Office
11、r, Naval Aviation Supply Depot, Philadelphia 20, Pennsylvania, Attention Code OPT). Bircraft Piloted Aircraft Copies of this specification and applicable specification may be obtained 3. REQIFEMEhTS 3.1 sufficiently complete to expedite a prompt investigation and review of the derived performance an
12、d to permit additional calculations to be made by Bar personnel as required. 3 e1.1 BASIC DATA.- Prior to proceeding with the initial performance calculations for the Standard operational weight limitation; mexirmUn allowable load factors at take-off, combat and design weights, etc. (3) wer plant se
13、a level static thrust or power ratings, specific fuel consumption ratings and indude source of ratings (applicable engine specification). 3.1.2.1.3 ABcp)pNAMIC DATA.- Present an analysis leading to the establishment of all lift and drag values used in the calculations inclMing any corrections mede t
14、o obtain trimmed lift and drag. incremental drag for speedbrakes, feathered propeller, wind- milling propeller, cowl flaps, and in operative engine (both jet and reciprocating), aa applicable, shall be shown. Included also shall be the following graphs: (1) Drag polars for the airplane trimmed in th
15、e clean, takeoff, and landing con- fiwations (out of grouad effect) BB shaun in Figure 1 and 3. Ekample is shown in Figure 15. Example is shown in airspeed for stall or minimum usable flying speed, as applicable vs 3 Licensed by Information Handling ServicesMILP-22203 ( Aer) (a) Clean configuration
16、without power (b Landing configuration without power (c/ Landing configuration with approach power (d Take-off Configuration with take-off power Example is shown in Figure 18 Take-off distance vs gross weight for both ground run and distance over 50 foot obstacle at sea level on stardard day in calm
17、 air for land and carrier based aircraft. In the absence of flight test data, take-off distance for turbo-jet aircraft shall be based on take-off speed which is not less than 1.2 times power-off stall speed in take-off configurtion and shall be shown for military ard n!aximum thrusts. weight at sea
18、level on standard day under calm wind and water comiitions. Example is shown in Figure 19. Landing distance vs weight for both ground run ad distance over 50 foot obstacle at sea level on standard day in calm. data, landing distance shall be based on touch down speed which ia not less than 1.2 times
19、 parer-off stall speed in landing configuration. acceleration for turbo-jet powered aircraft at 35,000 feet altitude anl two higher altitudes. (12) Level flight longitudinal acceleration vs true airspeed for take-off con- figuration at ambient temperatures of 59OF and 899 at normal and maximum allow
20、able take-off gross weights. For aircraft having more than one external configuration, effects of drag at various weights are desired. Examples are shown in Figures 22 to 26 inclusive. (9) For seaplanes, plot take-off tim vs take-off (10) In the absence of flight test (il) Normal acceleration vs tru
21、e airspeed for various rates of longitudinal Example is sham in Figure 20, Example is shown in Figure 21. (13) For all calculations involving fuel flow, engine specification fuel consumption data shall be increased by 5% for service use. Flight test fuel consumption data shall not be increased, howe
22、ver, All graphs presenting fuel flou or range data shall reference source of fuel con- sumption data ard whether increased by 5%. Ratsof-climb data shall be corrected for accelerating or decelerating effects of varying climb airspeeds with altitude. 3.1.2.1.7 CARRTER SUITABILITY.- For carrier based
23、aircraft, a detailed analysis of airplane launching characteristics that are in agreement with the minimum wind requirements of paragraph 3.4.2.1(a) of MIGc-501lA should be submitted in a separate report. This procedure is intenled to avoid delay in the submittal of the substantiating data for the S
24、AC charts. 3.1.3.1.8 bothrendezvous missions with tanker and/or Biiddy type refueling. tanker radius and fuel available for transfer may be obtained from BuBer (AD-33). 3.1.2.1.9 REFERENCE MATRuIL.- All reference material concerning the preparation of prepared by the Contractor and not previously su
25、bmitted, should be included as an appendix to the substantiating Performance Data Report. 3 -2 MISSIONS.- Combat rsdius and endurance problems for combat ab patrol, low- and high-altitude photographic, special store deliv.ery (sea level and 15,000 feet altitule) and in-flight refueling missions of j
26、et aircraft are contained in Appeiadix I of this Specification. supplement the problems of Table I of MILC-501IA. IN-FLIGHT FEFUELMG.- It is required that SAC chart submittals far receiver aircraft having in-flight refueling (IFR) capabilities inclde iFR radii for Information concerning tho substant
27、iating data report should be tabulated and any specific material These problems are intended for use in preparation of SAC charts and 4- QUALITY ASSWCE PROVISIONS 4.1 INSPECTION ANII ACCE?TTANCE.- The Perfornaance Data Report will be subject to final inspection and approval of the BITAEX as required
28、 by 1.iIL-D-8706. 811 4 Licensed by Information Handling Services5.2.1 MIL-P-22203 TM E 7777906 0225275 7 MILP-22203 ( Aer) data contained in this report are subject to review and analysis and shall be closely coordinated with BUAER (AD-33). 5. PREPARATION FCR DELIVERY 5.1 not be folded. copy of the
29、 ap2licable letter of transmittal. 5.2 ?ACKING.- Reproduction copy shall be packed separately and in such manner that contents will not be damaged during shipment. Reproduction copy shall All shipping containers containing reproduction copy shall also contain a MARKING AND LABELNC.- All shipping con
30、tainers shall be addressed to: Bureau of Aeronautics Department of the Navy Washington 25, D. C. Attn: AD-33 The following inforination shall appear on all shipping containers for reproduction copy: Reproduction Copy “Government Order No. (or Contract No.)“ 6. NOTES 6.1 INTEE?HETATION.- Interpretati
31、ons of the technical requirements of this documsnt may be obtained from BINER. NOTICE: When Government drawings, specifications, or other data are used for any purpose other than in connection with a definitely related Government procurement operation, the United States Government thereby incurs no
32、responsibility nor any obligation whatsoever; and the fact that the Government may have formulated, furnished, or in any way sup?lied the said drawings, specifications, or other data is not to be regarded by implication or otherwise as in any manner licensing the holder or any other person or corpor
33、ation, or conveying any rights or perniission to manufacture, use, or sell any 2atented inventions that may in any way be related thereto. 5 Licensed by Information Handling ServicesLicensed by Information Handling Services MIL-P-22203 Til W 7777706 0225277 O W MILS22203 (Am) Licensed by Information
34、 Handling ServicesMIL-P-22203 Til W 7797706 0225278 2 W a Licensed by Information Handling ServicesMIL-P-22203 Til 777770b 0225277 B 122203 ( Aer ) I 1- 9 Licensed by Information Handling ServicesMIL&22203( Aer) . . . . 10 Licensed by Information Handling ServicesMIL-P-22203 TM U 777770b 0225281 2 U
35、 MlLP-22203( Aer) . . . - - Licensed by Information Handling ServicesMIL-P-22203 TU m 777770b 0225282 L) m MGP-22203 ( Aer ) Licensed by Information Handling ServicesPIL-P-22203 TM 779770b 0225283 b MIGP-22203( Aer) Licensed by Information Handling ServicesMIL-P-22203 TM W 777770b O225284 W MIGP-222
36、03 ( Aer Licensed by Information Handling ServicesMIL-P-22203 TU = 777778b 0225285 T W MIG F 22203 ( Aer Licensed by Information Handling ServicesMIL-P-22203 TM m 7797706 0225286 L I( MIGP-22203 ( Aer ) Licensed by Information Handling ServicesI MIL-P-22203 Til W 9999706 0225287 3 II MZ-F-222031 ber
37、) 17 . Licensed by Information Handling ServicesMIL-P-22203 TM 777770b 0225288 5 - W Licensed by Information Handling ServicesU M&P-22203( Aer) MIL-P-22203 Til W 9799706 0225289 7 mi Licensed by Information Handling Services- Licensed by Information Handling Servicesi ! MIL-P-22203 TM 777770b 022529
38、1 5 W MfGP22203 ( Aer ) 0 Licensed by Information Handling Services4 . e. - .I , - _._ Licensed by Information Handling Services4 I f *- I MIL-P-22203 TM 7797706 0225273 7 m! MILP.22203 ( Aer ) Licensed by Information Handling Services,- ?I MIL-P-22203 TM m 7777706 0225274 O = MILP-22203( Aer ) -. L
39、icensed by Information Handling ServicesI MIL-P-22203 TM m 7977706 0225275 2 m MfGP-22203( Aer) 25 Licensed by Information Handling ServicesI- - MIL-P-22203 Til W 7777906 0225276 Y W Licensed by Information Handling Services,*- .I MIL-P-22203 TM 777770b 0225277 h MILSz!223 ( Aer ) Licensed by Information Handling ServicesMIL-P-22203 TM m 777770b 0225278 8 m MIGP-22203(Aer 1 J Licensed by Information Handling Services4 MIL-P-22203 ( Aer) .- Licensed by Information Handling Services
