1、 I o NIL-T-18232B 15 = 7779706 Oq25418 b 47 1. o MIL-T-l8232B(AS) 22 March 1968 Superseding MIL-D-18232 ( Ae r ) 2 September 1959 MILITARY SPECIFICATION GEHERAL SPECIFICA!i!IO FOR TARGETS, AERIAL, POWERED,DESIGN AND CO“RUCII0N OF This specification has been approved by the Naval Air Systems Cmand, D
2、epartment of the Navy. 1. SCOPE 1.1 the design and construction of-aerial powered targets, other than converted air- craft targets. SCOPE. - This specification embodies the general requirements of the Naval Air Systems Canmand Headquarters (NAVAIR) for The following shall apply to the specific targe
3、t concerned: Navy model designation Designers nime Designer s Model designation Eirmiber an kind of engine(s) 1.1.1 1.2 MISSION. - The mission of the target shall be a8 specified in the type or detail specification. CLASSFCO. - Targets designed and constructed under this speciflcation are classified
4、 as follow: (a) ri mental. (b) Developmental. (c) Prototype. (d) Production. 2.1 OF -. - !Che foilawing specifications, invitation to bid unless otherwise specified in the type or detail epecification shall form a part of this specification, except that later revisions of material and procesa specif
5、ication6 may be wed subject to approval by the local government representative. (LGR) without change in any terms of the contract. standad8 and drawings of the issue in effect on date of fod FSC-15 5 O u Licensed by Information Handling Servicesm-T-l8232B( AS) 2.1.1 MILITARY MIL-P-116 MIL- B- 5 087
6、MIL-E-5400 MIL-“- 5422 MIL-P-5518 MIL-F-5572 MIL-T-5579 MIL-0-5606 MIL- 5-5624 MIL- V- 5636 MIL-C-5637 MIL-E-6051 MIL- 1-6181 MIL-T-6396 Mn;-E-7016 MIL-1-7171 MIL-F-7179 MIL-C-7244 MIL-R-7705 MIL-E-7729 MIL-S-7742 MIL-T-7743 MIL-L-O MIL-W-8160 1-8189 MIL-I-OO MIL-A-8591 MIL- 5-8667 1-8678 MIL-H-8775
7、 MIL-D-8804 MIL-A-8870 SPECIFICATIONS Preservation, Methods of Bonding, Electrical, and Lightning Protection, for Aerospace System Electronic Equipment, Aircraft, General Specification for Teeting, environmental Electronic Equipment Pneumatic System; Aircraft Design, Installation and Data Require- G
8、asoline, Aviation Tanks; Self-sealing Oil, Aircraft Hydraulic Fluid, Petroleum Base, Aircraft and Missile, and Ordnance Turbine Fuel, Aviation, Grades JP-4 and Jp-5 Valve, Lubricating Oil Cooler, Petroleum Base, Temperature Regulating Coolers, Lubricating Oil, Aircraft, Tubular Electrical-Electronic
9、 System Compatibility and Interference Control Requirements for Aeronautical Weapons Systems, Associated Sub- systems and Aircraft Interference, Controlled Requirements, Aircraft Equipment Tanks, Fuel, Oil, Water-Alcohol, Collant Fluid, Aircraft, Non-Self - Electrical Load and Power Source Capacity,
10、 Analysis of; Method for Insulation Blanket, Thermal-Acoustical Finishes and Coatings: General Specification for Protection of Aero- Cap and Adapter Unit, Tank Filler Radomes, General Specification for Enamel; Gloss Screw Threads, Standard, Optimum Selected Series: Gen. Spec for Testing: Store Suspe
11、nsion Equipment General Specification for Lubricating Oil, Aircraft Turbine Engine, Synthetic Base Wiring, Guided Missile, Installation of, General Specification for Electronic Equipment, Guided Missiles, General Specification for Interchangeability and Replaceability, of Component Parts for Airborn
12、e Stores and Associated Suspension Equipment; General Design Jet Assisted Take-off Units-Installation of; in Naval Aircraft Cooling Requirements of Power Plant Installation Hydraulic System Components, Aircraft and Missiles, General Specifi- De-Icing System, Pneumatic Boot, Aircraft, General Specifi
13、cation for Airplane Strength and Rigidity Vibration, Flutter and Divergence ments for with Surge Protection Sealing, Removable, Internal Aircraft and Missiles space Weapons Systems, Structures and Parts Aircraft and Missiles Criteria for cation for 2 -. Licensed by Information Handling Servicesr. MI
14、L-T-L232B 25 m 7977706 0425420 4 m E 1-T-18232( AS) 2.1.1 MILITARY MIL-F-17874 MIL-c-18263 MIL-N-18307 MIL-H-18325 MIL-F-18372 MIL-1-18464 MIL-T-lw MIL-1-18802 1-21625 MIL-R-22449 -E23699 MIL-P-24014 MIL-P-25062 MIL-E-25366 MIL-H-25 475 ME#-P-26366 Ont (cont Fuel Systems: Aircraft, InstaUation and T
15、est of Colors, Exterior, Naval Aircraft; Requirements for Nomenclature and Nameplates for Aeronautical Electronic and As soc iat ed Equipme nt Heating and Ventilating Systems, Aircraft;, General Specifica- tion for Flight Control Systems: Design, Installation and Test of, Aircraft (Gen. Spec. for) I
16、nsignia and Markings for Naval Weapons System Thermal Anti-Icing Equipment, Wing and Ebpennage mel and Oil Lines, Aircraft, Installation of Design and Evaluation of Cartridges (For Cartridge Actuated Requirements (Certification) Br Pyrotechnic Item Lubricating Oil, Aircraft Turbine Engines, Syntheti
17、c Base Preclusion of Hazards from Electromagnetic Radiation to Ordnance Parachute Recovery Systems, Missile and Drone, General Electric and Electronic Equipment and Systems Guided Missiles, Hydraulic Systems,Missile,Design, Installation, Tests and Data Propeller Systems, Aircraft, General Specificat
18、ion for Devices) Requirements for Development of Installation of, General Specification for WONS SPECIFICATION WS-4235 ws-4613 Rocket Thrust Unit, Air Launched, Development Requirements for Safety Requirement Minimum for Aerial Target WEAPON RJQ- WR-62 Naval Weapon Requirements Specifications and St
19、andards: Use of MILITARY MIL-STD-129 MIL-STD-210 MILI-STD-704 MIL-STD-O MIESTD- MIL-HDBK-5 MIL-HDm-217 . L Marking for Shipment and Storage Identification Marking of U.S. Military Property Climatic Extremes for Military Equipment Electric Power, Aircraft, Characteristics and Utilization of Lubricati
20、on of Military Equipment HAMI- Strength of Metal Aircraft Elements Reliability, Streas and Failure Rate Data for Electronic EQw?=nt 3 Licensed by Information Handling ServicesNIL-T-L82328 15 m 9999906 OLi2542L b m MIL-T-l8232B( AS) 2.1.1 (cont ) ANC-18 mc-19 Design of Wood Aircraft Structures Wood A
21、ircraft Inspection and Fabrication (When requesting applicable documents, refer e0 both title and number. Depot, 5801 Tabor Avenue, Philaelphia, Pennsylvania 19120.) 2.1.1.1 OTHER. - Other Government specifications applic- able to the design and construction of aerial powered targets, in the LIST OF
22、 MILITARY SPECIFICArpIONS AND SIPANDARDS USED BY TRE NAVAL AIR SYSTEMS Copies may be obtained from the Conmianding Officer, Naval Supply COMMAND, NAVAIR -25-5446 2.1.2 STANDARDS. - Government standards applicable to the list specified in 2.1.1.1. the design and construction of aerial parered targets
23、, in 2.1.3 DRAWNGS. - Government drawings applicable to the LIST OF AEXONATICAL Sw DRAWINGS USED BY THE NAVAL AIR SYSTWS Cm, 2.1.4 SUPPLY CA!MLOGS OF NAVY MATERIAL. - Standard stock items as listed in bold face type in the Supply Cataloga of Navy Material shall be considered for use in all cases whe
24、re applicable; however, the use of improved equipment and materials is desired and encouraged. the design and construction of aerial powered targets, in NAVAIR 00-25-543 2.2 USE OF SPECIFICATIONS AND STANDAFUS. - Use of specifications WR-62. cations shall be approved or released by NAVAIR, except fo
25、r those documents for which authority has been delegated to the LOR (local Government representative). Contract or documents approved by NAVAIR or LCR ehall not be changed without prior approval of the respective approving authority. Approval of contractor documents for a specific contract shall not
26、 constitute approval for other contracts held by the same contractor or for contracts held by other contractors. publications refer to both title and number. applicable specifications, standars, drawings, and publipations may be obtained upon application to the Commanding Officer, Naval. Supply Depo
27、t, 5801 Tabor Avenue, Philadelphia, Pennsylvania 19120) . 3. REQUIIWlENTS and standards by design activities shall be in accordance with Contract documents unless otherwise specified by applicable design specifi- (When requesting specifications, standards, drawings, and Copies of this specification
28、an 4 - Licensed by Information Handling ServicesMIL-T-182329 15 H 7777706 O425422 H 3 .I the mission of the target as specified. coordinated and integrated to enable the required over-all target performance to be accomplished with the highest practicable degree of effectiveness. TARGEZ. - Each aeria
29、l powered target shall be designed and constructed to efficiently serve a6 the vehicle to accomplish The design of the target shall be 3.1.1 CHARACPERISTICS. - Characteristics of the target shall consist gravity locations, areas, dimensions and general data, and control surface movements. of the tar
30、get configuration, performance, weights, center of 3.1.1.1. TARGEZ CONFIGURATION. - !Three-view drawings of the target When applicable, separate drawings showing (1) target less JATO mediums and (2) target with JATO mediums attached shall be furnished. The drawings shaU be to such scale that the thr
31、ee views can be clear1y.show-n on a letter size page and that the distinguishing characteristics of the design are readily recognized. The following dimensions ahall be indicated on ;the drawings: span of wings, over- all length, and over-all height. 8 x 1042 inches shall be inserted in the detail s
32、pecification. 3.1.2.1 GUARAHPEED PERFORMANCE. - Guaranteed performance at specified gross weights shall be as specifled by the detail specifica- tion. Perfonnance curves shall be included for airspeed, altitude and endurance at gross weight and empty weight. be provided when applicable. External sto
33、re performance curves shall also 3.1.2.2 fication, with 3.162.3 specification. 3.1.3 specified. 3.1.3.1 SPECIFIC FUEL CONSIMPTIOR. - Performance shall be based on the specific fuel consumptions specified in the engine speci- inetallation losses . RAIIAR CROSS-SECTION. - Guaranteed raar cross-section
34、, both uuaugmented and augmented shall be as specified in the detail WEICtHTs. - WeigMs shall consist of gross weights, mission loade, and weight empty. Guaranteed weight shall be as GRW WEIGHT. - The gross weight is the sum of the mission losd and the weight ety. Separate gross weights for the laun
35、ching conition and the noma flight condition shaU be.inserted where applicable 3.1.3.2 and miscellaneous. 3.1.3.2.1 MISSION LOAD. - Mission load ahall consist of specified com- binations of fuel, oil, payload both intenial and external, HIEL. - Fuel shall be considered to be in categories as follows
36、: (1) Internal, (2) External, an (3) Unusable. 5 Licensed by Information Handling ServicesMIL-T-18232B 15 W 7777906 OLi25Li23 T W 1-T-18232( AS) 3.1.3.2.2 3 ei.3 e2.3 or detail specification. OIL. - Oil shall be considered to be in categories as follows: (i) Engine an (2) Unusable. ELECTOMC AND ELEC
37、TRICAL INSTAUATIONS. - The electronic and electrical installations shall be as specified by the type 3.1.3.2.4 required for the nod operation of the target is included in mission load. Flight test instrumentation and telemetry used for experimental or flight demon- stration purposes may replace part
38、 of the mission load with the approval of NAvm. MSTRMEIKCATION. - Instrumentation shall be as required by the type or detail specification. Instrumentation that is 3.i.3.2.5 specification and shall consist of items of a miscellaneous nature, such as pay- load and recovery system. MScELLANEoUS EQIPME
39、NT MSTALLATION. - The miscellaneous equipnt installation shall be as specified by the detail 3mie3e2.6 UNIT WEIGHTS OF MISSION M)AD me - The fOllawiw unit weights shall be wed in calculating mission loads. FUEL WEIGHLI (per ion) Specification MiL-F-5572 Aviation Gas Specification MIL-J-5624, Grade J
40、P-5 fuel Other fuels 6 pounds 6.8 pounds EMIRAULIC FLUID (per gallon) MIL-H-8775 7.0 pounds 7.4 Pow* OIL WEIGHT (per mon 8.0 pounds 3.1.3.2.7 MISSION LOAD CONDTIONS. - Mission load conditions shall be other important missions of the target. Miesion load shall be sitbdivided as follom: Specification
41、MIL- 5-4624, JP-4 fuel 6.5 chord line) Height over highest fixed part of or propeller aisc) Reference line level (reference On Wing truck Height over hiaestpart of tail, Height in hoisting attitude, from sling to lowest part of target target (wing, tail is to 1: reference line level top of hoisting
42、m-T-18232( AS) degrees - degrees - feet percent feet percent percent - - - percent percent - feet inches - percent degrees - degrees degrees degrees - percent - degrees feet feet feet feet - - Licensed by Information Handling ServicesI i I l MIL-T-L232B 15 W 777770b 0425427 7 9 1L-T-18232( AS) 3.1.6
43、 ( Cont ) Length, msximum: Reference line level On handling truck feet feet - Length from hoisting sling to farthest after part of tail, reference line level, rudder neutral, elevator down feet - Distance from wing mean aerodynamic quarter-chord point to horizontal tail mean aerodynamic quarter-chor
44、d point Distance from wing mean aerodynamic quarter-chord point to vertical tail mean aerodynamic quarter-chord point Propeller clearance (normal) : Reference line level feet - feet inches - feet - Propeller diameter 3.1.7 COrJTROL SURFACE MOVEMENTS. - Control surface movements on by stops shall be
45、as specified in the detail specification. (Not to be used for inspection purposes.) each side of neutral position for full movement as limited degrees rigt degrees left - degrees right degrees left degrees above Rudder Rudder tab or trim surface degrees below Elevators or movable stabilizer Elevator
46、s tab or trim surface degrees above degrees below Ailerons degrees above degrees below Aileron tab degree8 above degrees below - - 3.1.8 SMPLICTPY. - The design shall provide for a maximum of simplicity conunensurate with other criteria. 10 Licensed by Information Handling ServicesM1-T-1823213( AS)
47、3.1.9 RELIABILITY. - Numerical. reliability and confidence levels of aspects: the target system shall be specified following operational (i) Checkout reliability. - Checkout reliability mans the probability, numerically expressed, that any randomly selected target will pass all prescribed checkouts
48、required to prepare the target for launching without necessity for repair or replacement of componente. Minor adjustments which may be required during these checkouts will not be con- sidered as deviations to this requirement. pass all prescribed checkouts prior to the first launching, due to establ
49、ished defects in workmanship or material shall be reworked as necessary at contractor expense in order to pass all prescribed checkout requirements. Targets which do not successfuly (2) Flight reliabilitx, - Flight reliability means the proba- bility, numerically expressed, that any target randamly selected from targets which have passed the ready storage checkout, shall operate in the launch phase and free flight phase in accordance with the guaranteed performance requirements. (3) Recovery reliability. - Recovery r
