2024年2月27日 · This section provides the design considerations, requirements, and examples for the following hardware and equipment: Tools, Drawers and Racks, Closures and Covers, Mounting Hardware, Handles and Grasp Areas, Restraints, Mobility Aids, Fasteners, Connectors, Windows, Packaging, Crew Personal Equipment, and Cable Management.

2025年2月18日 · Requirements in this section apply to all hardware and equipment with which the crew interfaces—from large and complex systems such as ISS racks, to small items such as tools, drawers, closures, restraints, mobility aids, fasteners, connectors, clothing, and crew personal equipment.

2021年9月30日 · This document is directed toward Materials and Processes (M&P) used in the design, fabrication, and testing of flight components for all NASA manned, unmanned, robotic, launch vehicle, lander, in-space and surface systems, and …

2020年4月1日 · NASA Manufacturing and Test Requirements for Normally Closed Pyrovalves for Hazardous Flight Systems Applications

This NASA Technical Standard is directed toward materials and processes (M&P) used in the design, fabrication, and testing of space program flight hardware for NASA, including but not limited to crewed, uncrewed, robotic, launch vehicle, lander, in-space and surface systems, and

2021年8月6日 · This NASA Technical Standard establishes criteria for ensuring the integrity of threaded fastening systems in launch and space vehicles and their associated equipment. Requests for information should be submitted via “Feedback” at https://standards.nasa.gov.

2021年8月6日 · The purpose of this Standard is to specify requirements for design and analysis of threaded fastening systems in NASA spaceflight hardware.

2021年8月21日 · The purpose of this NASA Technical Standard is to establish minimum requirements and provide effective guidance regarding methodologies and best practices for testing systems and hardware to be exposed to dust in …

2021年3月12日 · Using risk-informed selection and use of the requirements, controls, and practices, herein, that maximize conformance of hardware attributes and process attributes considered to be critical for meeting mission success objectives.

This document is intended to cover analyses representing all phases of spaceflight hardware life cycles, including pre-flight, post-flight, and abort activities. The requirements herein represent the minimum set of conditions necessary to ensure proper identification of bounding loads and