AIR FORCE - 02 - Air Force Network Integration Center (AFNIC)

SMC-S-005

Thu, 01 Jan 2009 00:00:00 GMT

SMC-S-005; SPACE SYSTEMS – FLIGHT PRESSURIZED SYSTEMS AIR FORCE - 02 - Air Force Network Integration Center (AFNIC) This document establishes the baseline requirements for the design, fabrication, assembly, installation, test, inspection, operation, and maintenance of pressure systems used in spacecraft and launch vehicles. It deals primarily with the interfaces between the pressure vessel(s), or pressurized structures, and the corresponding pressure components within a specific pressure system; and interfaces between a pressure system and other spacecraft or launch vehicle systems. These requirements, when implemented on a specific pressure system, will assure a high level of confidence in achieving safe and reliable operation.

DOD-E-8983C

Sat, 01 Jan 1977 00:00:00 GMT

DOD-E-8983C; ELECTRONIC EQUIPMENT, AEROSPACE, EXTENDED SPACE ENVIRONMENT, GENERAL SPECIFICATION FOR AIR FORCE - 02 - Air Force Network Integration Center (AFNIC) This specification sets forth the general requirements for the design and manufacture of electronic components and equipment for space vehicles. The detailed performance and individual test requirements shall be as specified in the equipment specification or the contract. Beneficial comments (recommendations, additions, deletions), and any pertinent data which may be of use in improving this document should be addressed to:

           SAMSO/AW            P.O. Box 92960, Worldway Postal Center,            Los Angeles, CA 90009

Use the self-addressed Standardization Document Improvement Proposal (DD Form 1426) appearing at the end of this document or comment by letter.
The requirements covered by this specification are applicable to electronic components and equipment to be used on space vehicles (see 6.1). This specification may also be used as a reference document to specify general requirements for electronic components to be used on launch vehicles, intercontinental ballistic missiles, or other vehicles. For those applications the term "space vehicle" is to be interpreted as the applicable vehicle.

SMC-S-017

Tue, 01 Jan 2008 00:00:00 GMT

SMC-S-017; LITHIUM-ION BATTERY FOR SPACECRAFT APPLICATIONS AIR FORCE - 02 - Air Force Network Integration Center (AFNIC) Purpose
This document establishes standards for the development, testing, storage, handling, and usage of lithium-ion batteries for military spacecraft. Compliance with this standard is intended to assure proper performance of batteries and to provide protection against pre-flight degradation and premature degradation during operational use on space, launch, and upper-stage vehicles.
Application
This report is intended for compliance in applicable military spacecraft acquisition and development to incorporate common requirements and practices necessary to assure successful lithium-ion battery operation during space missions. It is expected that battery piece parts, such as cell, cell-module, charge control electronics, bypass switch, heaters, temperature sensors, etc., are procured to lowerlevel qualification documents that define design, process, and quality controls, and qualification and acceptance test requirements.
Conflicts with Other Standards
In the event of conflict between this document and the AIAA Electrical Power Systems for Unmanned Spacecraft Standard1 or the Space Battery Standard,6 this document shall take precedence with regards to any battery-specific definition or requirement.

MIL-STD-1540D

Fri, 01 Jan 1999 00:00:00 GMT

MIL-STD-1540D; PRODUCT VERIFICATION REQUIREMENTS FOR LAUNCH, UPPER STAGE, AND SPACE VEHICLES AIR FORCE - 02 - Air Force Network Integration Center (AFNIC) This document requires that a process be established to develop and manage verification requirements to assure that launch and space equipment can function correctly and withstand stresses it may encounter during its life cycle including end-of-life performance requirements. This document is intended for use in developing the detailed verification requirements for a particular project. The application of these requirements should result in an effective verification process and consequently high confidence in achieving successful space missions.