1、 MIL-R-85545B 33 W 9797906 0463909 7 W . -i - I INCH-POUND I MIL-R-85545B(AS) 30 November 1990 SUPERSEDING 4 April 1986 MIL-T-85545A(AS) MILITARY SPECIFICATION ROCKET, GTR-18A This specification is approved for use by the Naval Air Systems Command, Department of the Navy, and is available for use by
2、 all Departments and Agencies of the Department of Defense. 1. SCOPE 1 . 1 Scope. Thl s spec! fl cati on establ i shes the requi rements for the manufacture and inspection of the GTR-18A rocket referred to herein as the rocket. 2. APPLICABLE DOCUMENTS 2.1 Government documents. 2.1 . 1 Sgeci fi catio
3、ns. standards. and handbooks. The fol 1 owl ng specifications, standards, and handbooks form a part of this document to the extent spec! fi ed here1 n. documents are those listed in the issue of the Department of Defense Index of Specifications and Standards (BODPSS) and supplement thereto, cited in
4、 the solicitation (see 6.2). Un1 ess otherwi se apeci fied, the l ssues of these SPECIFICATIONS MILITARY MIL-1-85549 STANDARDS MILITARY MIL-STB-129 MI L-SPB-81 O Envi ronmental Test Methods and Engineering MI L-STB-1169 Ammuni %ion Data Card MI L-STD-1168 Marking for Shipment and Storage Gui del i n
5、es Atnmunl ti on Lot Number! ng Igniter, PVU-3A/E and PVU-3B/E Beneficial comments (recommendations, addl ticans, deletions) and any pertinent data whlch may be of use ln improving this document should be addressed to: Naval A4 r Eng! neeri ng Center, Systems Eng1 neeri ng and Standardization Depart
6、ment. (Code 531, bakekurst, NJ 08933-5900, by using the Standardization Document Improvement Proposal (DB Form 1426) appearing at the end of this document or by letter. AMSC N/A FSC 1370 DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited. Licensed by Information Handlin
7、g ServicesMI L-R-85545B(AS) (Unless otherwise indicated, copies of federal and military specifications, c tandards, and handbooks are avai 1 ab1 e from the Standardization Documents Order Desk,Building 4D, 700 Robbins Avenue, Philadelphia, Pa 1911-5094, 2.1 .2 Other Government documents, drawi nqs ,
8、 and pub1 i cations. The fol lowi ng Unless otherwise specified, the issues other Government documents, drawings, and publications form a part of this document to the extent specified herein. are those cited in the solicitation. DRAW I NGS NAVAL AIR SYSTEMS COMMAND (NAVAIR) (CAGE Code 30003) 1335AS2
9、75 1335AS280 1335AS285 1335AS289 1335AS290 1335AS380 1335AS390 1335AS700 Igni ter, PVU-3A/E Rocket, GTR-18A Decal, GTR-18A Smokey Sam Rocket Shipping Condi tion Packaging Assembly Launcher, Rocket LMU-23AIE Simulator, Surface-to-Air Missile SMU-l24/E (Smokey SAM Simulator) Launcher, Rocket LMU-24A/E
10、 (Un1 ess otherwi se indicated, Copi es of Naval Air Systems Command drawings are available from the Naval Air Technical Services Facility (NATSF) (Code 312) , 700 Robbins Avenue, Philadelphia, Pa 19111-5096. ) PUBLI CATIONS CODE OF FEDERAL REGULATIONS 49 CFR 100-1 99 Transportati on (Copies are ava
11、ilable from the Superintendent of Documents, U.S. Government Printing Office, Washington, D.C. 20402-0001 .) NAVAL AIR SYSTEMS COMMAND 1 1-75-63 Techni cal Manual for LMU-23A/E and LMU-24A/E (Copies are available from the Naval Publications and Forms Center (Code lOSl), 5801 Tabor Avenue, Philadelph
12、ia, PA 19111-5099,) 2.2 Order of precedence. In the event of a conflict between the text of this document and the references cited herein, the text of this document takes precedence. regulations unless a specific exemption has been obtained. Nothing in thi s document, however, supersedes appl i cab1
13、 e laws and 3. REQUIREMENTS 3.1 First article. When specified (see 6.21, a sample shall be subjected to first article inspection (see 6.4) in accordance with 4.4. 3.2 Desiqn and construction. accordance with Drawing 1335AS280. rocket, see Drawing 1335AS390. The rocket shall be fabricated and assemb
14、For the smokey SAM simulator, uti 1 izing 2 ed in the Licensed by Information Handling ServicesMIL-R-S5LI5B 13 I 77977Ob OLibLSLL 5 I f MI L-R-85545 B (AS 3.3 Environmental conditioninq. The rocket shall withstand exposure to vibration and shock without performance failure (see 4.6.2 and 4.6.3). 3.4
15、 Performance. The rocket shall meet the following requirements when launched at an angle of 80“ or 85“ (see 4.6.4): a. The rocket shall expel a visible flame and white smoke plume during powered flight (see 6.5.1). b. The rocket shall not impact the ground during powered flight. c. The rocket shall
16、attain an altitude of 1500 tl 500 ft. above launcher. 3.5 Marking. In addition to any special or other identification required by the contract (see 6.21, rockets shall be marked with lot numbers (see 4.5.3) on the designated area of the rocket decal, Drawing 1335AS285. 3.6 Data cards. Data cards sha
17、ll be prepared in accordance with MIL-STD-1167 and shall be furnished with each rocket lot (see 4.5.2). 3.7 WorkmanshiD. Workmanship and finish shall be in accordance with the highest grade practice used in manufacturing military weapons. Finished items and parts shall not exhibit poor material and
18、processing such as seams, laps, 1 ami nations, cracks, vi si ble steps, sharp edges, nicks, scratches, burrs, deformations, and missing operations which may affect serviceability, functioning, operation appearance, or safety. grease or any other foreign matter. materi al s on al 1 external surfaces.
19、 No part or assembly shall contain chips, dirt, 0 The rocket shall be free from explosive 4. QUALITY ASSURANCE PROVISIONS 4.1 Reseonsi bi 1 i ty for i nseection. Unless otherwi se specified in the contract or purchase order, the contractor is responsible for the performance of all inspection require
20、ments (examinations and tests) as specified herein. otherwise specified in the contract or purchase order, the contractor may use his own or any other facilities suitable for the performance of the inspection requirements specified here! n, unless di sapproved by the Government. Government reserves
21、the right to perform any of the inspections set forth in this specification where such inspections are deemed necessary to ensure suppl les and servi ces conform to prescribed requirements, Except as The 4.1.1 Reseonsi bi 1 i ty for compl lance. Al 1 i tems shall meet al 1 requi rements of section 3
22、 and 5. The inspection set forth in this specification shall become a part of the contractors overall inspection system or quality program. The absence of any inspection requirements in the specification shall not relieve the contractor of the responsi bi 1 i ty of ensuring that al 1 products or sup
23、plies submitted to the Government for acceptance comply with all requirements of the contract. Sampling inspection, as part of manufacturing operations, is an acceptable practice to ascertain conformance to requirements, however, thi s does not authorize submission of known defective material, eithe
24、r indicated or actual, nor does it commit the Government to acceptance of defective material. 4.2 Classification of inspections. The inspection requirements specified herein are classified as follows: 3 Licensed by Information Handling Servicest . Cumulative Sample Sample size sample size Accept lot
25、 1 16 16 O 2 13 29 1 3 13 42 2 MI L-R-85545B(AS) Cumulative interim reject 1 11 2 L/ a. First article inspection (see 4.4). b. Quality conformance inspection (see 4.5). 4.3 Inspection plan. Prior to first article or quality conformance inspection, the inspection plan (see 6.3) to be used for first a
26、rticle or quality conformance units shall be available to the acquiring activity. 4.4 First article inspection, First article inspection shall be performed on sample units which have been produced using the same materials, equipment, processes and procedures normally used in production. 4.4.1 Sample
27、. First article sample shall consist of 24 loaded rockets and 10 empty (devoid of all explosive material) rockets (see 6.4). 4.4.2 Inspection routine. The loaded rockets shall be divided into two groups of twelve. One group shall undergo in sequence, all the tests of 4.6 and the other group shall un
28、dergo only visual inspection (4.6.1) before ballistic testing (see 4.6.4). The empty rockets shall be inspected for conformance to 3.2 and 3.7. first article sample. 4.4.3 Failure. Failure of any rocket shall be cause for rejection of the 4.5 Quali tv conformance inspection. Quali ty conformance ins
29、pection shall consist of the tests specified in 4.6.1 and 4.6.4, in sequence. conformance inspections shall be performed on sample units produced from one lot. Quality 4.5.1 Samplinci plan. Sampling shall be as specified in table I. TABLE I. SamPlina plan, Rej ec t 1 ot 2 3 3 - 1/ Additional 13 samp
30、les shall be fired to prove acceptability of the lot. 4.5.2 m. A lot shall consist of rockets produced from one mix of propellant. 4.5.3 Lot numbering. Unless otherwise specified in the contract (see 6.2.11, lot numbering shall be in accordance with MIL-STD-1168. shall be assigned by the acquiring a
31、ctivity. Lot interfix numbers 4.6.1 Visual inspection. The rockets shall be visually inspected for conformance to the requirements of 3.2 and 3.7. be used for this inspection. Four power (4x1 magnification may 4 Licensed by Information Handling ServicesMIL-R-85545B 13 M 97779Ob OLIbL9L3 7 MI L- R-85
32、5458 (AS) 4.6.2 Vibration. While packaged in their shipping containers along with 12 PVU-3A/E igniters (see MIL-1-85547) according to Drawing 1335AS290, the rockets shall be subjected to a vibration test in accordance with MIL-STD-810, method 514.4, category 1. shall be used. . 0 Vibration test leve
33、ls given in figures 514.4-1 through 514.4-3 Test time shall be based on a transportation of 3,000 miles. 4.6.3 Shock. The rockets shall be removed from their shipping containers and subjected to a 6-foot drop test in accordance with MIL-STD-810, method 516.4, procedure IV. Drop height shall be measu
34、red from the lowest point of the test item to the impact plane. One-third of the rockets shall be dropped with the nose cone down, one-third with the nose cone up, and one-third with the longitudinal axis parallel to the impact plane. Drop orientation of the rocket shall be required at the release p
35、oint only. 4.6.4 Ballistic test. The rocket shall be fired in accordance with NAVAIR 11-75-63, Work Package 005 00, using an LMU-23AIE launcher (see Drawing 1335AS380) set at an angle of 80“ or an LMU-24A/E launcher (see Drawing 1335AS700) set at an angle of 85“ and a PVU-3AIE igniter (see Drawing 1
36、335AS275). The altitude of the rocket shall be measured. 4.7 First article or quality conformance inspection report. A first article or quality conformance report (see 6.3) shall be available to the acquiring activity within the time frame specified (see 6.2). fol lowing information: The report shal
37、l contain the a. Date of report b. Date of inspection c. Lot number d. Manufacturer e. Operational objective f. Test equipment used g. Environmental conditions at time of inspection or failure h. Type of failure, if any i. Analysis, significance, and recommendations j. Disposition of parts k. Correc
38、tive action taken because of failure 4.8 Inspection of packacring. packing, and container marking shall conform to this specification (see section 5). The sampling and inspection of the preservation, 5. PACKING 5.1 Preservation. Rockets shall be stored in a cool and dry environment until packed (see
39、 5.2). 5.2 Packing. Unless otherwise specified in the contract (see 6.2.11, rockets shall be packed in accordance with Drawing 1335AS289. rockets shall take place no later than 30 days after the rockets are removed from the curing ovens (see 5.1). Hermetic sealing of the 5.3 Marking. Unless otherwis
40、e specified in the contract (see 6.21, shipping containers and pallets shall be marked in accordance with MIL-STD-129 and the class B explosive, special fireworks requirements of 49 CFR 100-189. 5 Licensed by Information Handling ServicesMIL-R-85545B 13 U 9499906 0461914 O _ - MI L-R-85545B(AS) 6. N
41、OTES (This section contains information of general or explanatory nature 6.1 Intended use. The GTR-18A rocket is intended for use with the PVU-3A/E and PVU-3B/E igniters and the LMU-23A/E and LMU-24A/E launchers to train aviation and ground forces to recognize and cope with attacking surface-launch
42、missi les. 6.2 Acquisition requirements. Acquisition documents should specify the fol lowing: that may be helpful, but is not mandatory.) a. b. C. d. e. f. g- h, i. Title, number and date of this specification. Issue of the DODISS to be cited in the solicitation, and if required the specific issue o
43、f individual documrnts referenced (see 2.1.1). Part number. Quanti ty requi red. Whether first article is required (see 6.4), and if so, specify the test activity. Date and place of delivery. Packing, marking, and lot numbering, if other than specified in 3.5, 4.5.3, 5.2 and 5.3. Time frame for subm
44、ission of first article or quality conformance report. That the safety precaution requirements of the “Contractors Safety Manual for Ammuni ti on, Explosives , and Re1 ated Dangerous Materi al , II DoD 4145.26M are applicable. NOTE: When this specification is used as part of the description of work
45、to be accomplished by a Government activity, the safety precaution requirements of “Ammuni tion and Explosives Ashore,“ OP5 are applicable. 6 s hou aPP1 with prov spec requ 3 Consideration of data requi rements. d be considered when this specification is applied on a contract. The cable Data Item De
46、scridtions (DIDS) should be reviewed in conjunction the specific acquisition to ensure that only essential data are requested/ ded and that the DIDs are tailored to reflect the requirements of the fi c acquisition. rerct:lts, a Contract Data Reauirements List (DD Form 1423) must be wepared The fol l
47、owing data requirements To ensure correct Contractual application of the data II to .obtaiii the data, except where DOD FAR Supplement 27.475-1 exempts the requlrement for a DD Form 1423, Reference Paragraph DID Number DID Title Suggested Tai 1 ori ng 4.3 DI-NDTI-80566 Test pl an - 4.7 DI-T-2072 Rep
48、ort, test - The above DIDs were those cleared as of the date of this specification. The current issue of DOD 5010.12-L, Acquisition Management Systems And Data Requirements Control List (AMSDL), must be researched to ensure that only current, cleared DIDs are cited on the DD Form 1423. 6 Licensed by
49、 Information Handling Services- MIL-R-85545B 13 m 777770b 04b17L5 2 m MI L-R-85545B(AS) 6.4 First article. When a first article inspection is required, the item should be a first article sample. and 10 empty rockets. instructions in acquisition documents regarding arrangements for examinations, approval of first article test results and disposition of first articles. Invitations for bids should provide that the Government reserves the right to waive the requirement for samples for first article inspection to those bidders offering a product which has been previously acquire
