共找到 320 条与 航天器用能源设备 相关的标准,共 22 页
This document, when followed in its entirety, will yield a robust EPS design suitable for very high-reliability space missions. This document specifies general design practices and sets minimum verification and validation requirements for power systems of unmanned spacecraft. The focus of the document is on earth orbiting satellites using traditional photovoltaic/battery power, but does not exclude other primary power generation and storage methods. This document does not address specific launch vehicle requirements however much of the design philosophy used here is applicable to launch vehicle power systems.
Electrical Power Systems for Unmanned Spacecraft
本规范规定了空空导弹电源的通用要求、质量保证规定和交货准备等。 本规范适用于空空导弹电源(以下简称电源)的研制、生产和使用。
General specification for electrical power supply of air-to-air missile
A-A-59484, dated 14 March 2001, has been reviewed and determined to be valid for use in acquisition.
BRAKE MACHINES, SHEET METAL, MANUALLY OPERATED STANDARD AND BOX-PAN TYPE
This performance specification covers the general requirements for automotive valve regulated lead acid storage batteries(VRLA), also known as Sealed Lead Acid Batteries(SLAB). The batteries are nominal 12-volt batteries that are generally used for starting, lighting and ignition applications, have non-removable covers, and designed for maintenancefree operation.
BATTERIES, STORAGE: AUTOMOTIVE, VALVE REGULATED LEAD ACID (VRLA)
MS90384D, dated 18 January 2000, remains inactive for new design; however, the document is valid for use.
CABLE ASSEMBLIES, ELECTRIC POWER, PERMANENTLY WIRED, FOR PORTABLE GROUND SUPPORT TEST EQUIPMENT
This specification covers the general requirements for fixed (tapped and untapped) pulse delay lines.
DELAY LINES, ACTIVE, GENERAL SPECIFICATION FOR
MIL-T-152B, dated 24 May 2000, remains inactive for new design; however, the document is valid for use.
TREATMENT, MOISTURE AND FUNGUS RESISTANT, OF COMMUNICATIONS, ELECTRONIC AND ASSOCIATED ELECTRICAL EQUIPMENT
A-A-50506A, dated 06 August 2001, has been reviewed and determined to be valid for use in acquisition.
FAN, TUBEAXIAL, MINIATURE, FOR COOLING ELECTRONIC EQUIPMENT
This list has been prepared for use by or for the Government in the acquisition of products covered by the subject specification and such listing of a product is not intended to and does not connote endorsement of the product by the Department of Defense. All products listed herein have been qualified under the requirements for the product as specified in the latest effective issue of the applicable specification. This list is subject to change without notice; revision or amendment of this list will be issued as necessary. The listing of a product does not release or otherwise affect the obligation of the manufacturer to comply with the specification requirements.
BATTERIES, STORAGE, AIRCRAFT, GENERAL SPECIFICATION FOR
MIL-PRF-8565K, dated 25 June 2001, has been reviewed and determined to be valid for use in acquisition.
BATTERY STORAGE, AIRCRAFT, GENERAL SPECIFICATION FOR
A-A-50047A, dated 25 September 2001, has been reviewed and determined to be valid for use in acquisition.
DRY CLEANING UNIT ASSEMBLY, DRY TO DRY, PERCHLOROETHYLENE SOLVENT
This specification covers a forced draft and ventilation air personnel heater assembly, referred to as a “heater”(see 6.1).
HEATER ASSEMBLY, COMBUSTION VEHICULAR COMPARTMENT, 8.8/17.6 kW (30 000/60 000 BTU/HR) GENERAL SPECIFICATION FOR
This list has been prepared for use by or for the Government in the acquisition of products covered by Specification MIL-PRF-83532. Listing of a product is not intended to and does not connote endorsement of the product by the Department of Defense.
DELAY LINES, ACTIVE, GENERAL SPECIFICATION FOR
The General Services Administration has authorized the use of this commercial item description as a replacement for Military Specifications MIL-V-16720E and MIL-V-16721D which are cancelled.
DELAY LINES, PASSIVE, GENERAL SPECIFICATION FOR
This drawing describes the requirements for a family of 3-pin, single in-line package, passive delay lines.
DELAY LINES, PASSIVE, 3-PIN, SIP
This drawing documents five product assurance classes as defined in paragraph 1.2.3 and MIL-PRF-38534. A choice of case outlines and lead finishes which are available and are reflected in the Part or Identifying Number (PIN).
MICROCIRCUIT, HYBRID, LINEAR, MIL-STD-1553, BC/RTU/MT, MULTIPLEXED TERMINAL
This specification covers the general requirements for rechargeable, vented, nickel-cadmium aircraft storage batteries, cells, and all components (electrical and non-electrical) thereof.
BATTERIES AND CELLS, STORAGE, NICKEL-CADMIUM, AIRCRAFT GENERAL SPECIFICATION FOR
This standard establishes a test method standard for fuel cells and fuel cell fittings. This standard applies to all fuel cells manufactured in accordance with MIL-T-5578, MIL-T-6396 (except type I), and MIL-DTL-27422.
INSPECTION AND ACCEPTANCE STANDARDS FOR FUEL CELLS AND FITTINGS
The activities above were interested in this document as of the date of this document. Since organizations and responsibilities can change, you should verify the currency of the information above using the ASSIST Online database at http://assist.daps.dla.mil
ENGINEERING PRACTICES PRODUCTIVITY ENHANCEMENT OF INDUSTRIAL PLANT EQUIPMENT AND PRODUCTION SUPPORT SYSTEMS
This standard establishes qualification and quality requirements for solar cells. Section 7 describes specific tests necessary to ensure the quality and reliability of solar cells intended for space application. Section 8 describes specific tests necessary to characterize the performance of solar cells intended for space application. Section 9 describes the quality requirements for cells to be qualified to this standard. Section 11 describes the reporting format for the qualification tests in Section 7 and the data sheet characterizations in Section 8.
Qualification and Quality Requirements for Space Solar Cells
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