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(R2021) MIL-PRF-85046A_NOT_1-003.pdf
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(R2021) MIL-PRF-85046A_NOT_1-003.pdf
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PERFORMANCE SPECIFICATION
ACTUATOR, LINEAR, ELECTROMECHANICAL
This specification is approved for use by the Naval Air Systems Command and is available for
use by all Departments and Agencies of the Department of Defense.
1. SCOPE
1.1 Scope. This specification establishes the requirements for the manufacture and
inspection of one type of electromechanical linear actuator. The test limits in this specification
define minimum acceptable capabilities.
2. APPLICABLE DOCUMENTS
2.1 General. The documents listed in this section are specified in sections 3 and 4 of this
specification. This section does not include documents cited in other sections of this specification
or recommended for additional information or as examples. While every effort has been made to
ensure the completeness of this list, document users are cautioned that they must meet all
specified requirements of documents cited in sections 3 and 4 of this specification, whether or
not they are listed.
2.2 Government documents.
2.2.1 Specifications and standards. The following specifications and standards form a part
of this document to the extent specified herein. Unless otherwise specified, the issues of these
documents are those cited in the solicitation or contract.
DEPARTMENT OF DEFENSE SPECIFICATION
MIL-T-7743 Testing, Store Suspension and Release Equipment, General
Specification For
AMSC 9582 FSC 1095
INCH-POUND
Comments, suggestions, or questions on this document should be addressed to: Commander, Naval Air
Warfare Center Aircraft Division Lakehurst, Code 4.1.2, Mail Stop 120-3, Route 547, Joint Base MDL,
NJ 08733-5100 or emailed to michael.sikora@navy.mil. Since contact information can change, you may
want to verify the currency of this address information using the ASSIST Online database at
https://assist.dla.mil.
MIL-PRF-85046A(AS)
17 September 2015
SUPERSEDING
MIL-A-85046(AS)
7 September 1976
Source: https://assist.dla.mil -- Downloaded: 2021-08-10T11:55Z
Check the source to verify that this is the current version before use.
MIL-PRF-85046A(AS)
2
DEPARTMENT OF DEFENSE STANDARDS
MIL-STD-130 Identification Marking of U.S. Military Property
MIL-STD-461 Electromagnetic Emission and Susceptibility
Requirements for the Control of Electromagnetic Interference
MIL-STD-704 Aircraft Electric Power Characteristics
MIL-STD-810 Environmental Engineering Considerations and Laboratory
Tests
DEPARTMENT OF DEFENSE HANDBOOKS
MIL-HDBK-454 General Guidelines for Electronic Equipment
MIL-HDBK-1250 Corrosion Prevention and Deterioration Control in
Electronic Components and Assemblies
(Copies of these documents are available online at http://quicksearch.dla.mil or
https://assist.dla.mil.)
2.3 Order of precedence. Unless otherwise noted herein or in the contract, in the event of
a conflict between the text of this document and the references cited herein, the text of this
document takes precedence. Nothing in this document, however, supersedes applicable laws and
regulations unless a specific exemption has been obtained.
3. REQUIREMENTS
3.1 First article. When specified (see 6.2), a sample shall be subjected to first article
inspection in accordance with 4.2.
3.2 Design and construction. The design and construction of the actuator shall be in
accordance with the requirements specified herein. The actuator shall be capable of meeting all the
requirements of this specification after undergoing a room temperature shelf life of 48 months.
There shall be no repair of the actuator permitted to meet this requirement.
3.2.1 Materials. The materials shall be entirely suitable for the purpose intended. Materials
shall be selected on the basis of strength, workability, and compatibility with other materials in the
item so as to minimize galvanic action (see MIL-HDBK-1250). Mounting interfaces shall be
constructed of materials that are compatible with the cadmium plated steel pin pivots and stainless
steel nuts on the actuating ram.
3.2.2 Finishes. Finishes shall be applied to all materials, whenever applicable, and shall be
entirely suitable for the purpose intended, such as corrosion resistance and increased durability.
3.2.3 Surface texture. Surface texture shall not exceed 250 microinches (6.35 x 10
-8
Source: https://assist.dla.mil -- Downloaded: 2021-08-10T11:55Z
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MIL-PRF-85046A(AS)
3
centimeters) and there shall be no sharp edges or burrs.
3.2.4 Interchangeability. All actuators having the same part number shall be internally and
externally identical.
3.2.5 Identification of parts. All parts shall be marked as specified on the applicable
drawing or in accordance with MIL-STD-130, if not specified on the drawing.
3.2.6 Nameplates. Identification and wiring schematic plates for actuators shall be in
accordance with the applicable drawing for the actuator being procured.
3.2.7 Envelope.
3.2.7.1 Dimensions. The actuator envelope dimensions shall be in accordance with the
applicable drawing for the actuator being procured.
3.2.7.2 Electrical interface. The actuator cable interface shall be in accordance with
figure 1.
FIGURE 1. Actuator schematic diagram.
3.2.8 Weight. The maximum weight of the actuator shall be 1 pound (0.4536 kilogram).
3.2.9 Lubrication. If lubricants are used, they shall not be of a toxic nature or of such a
nature to cause injury to personnel.
3.2.10 Manual operation. The actuator shall incorporate provisions for a manual operation.
The ratio of turns of the manual input shaft to the actuating ram stroke shall be a maximum of 20
turns of manual input shaft rotation for linear movement of output shaft from fully extended to fully
Source: https://assist.dla.mil -- Downloaded: 2021-08-10T11:55Z
Check the source to verify that this is the current version before use.
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