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AIAA S-102.1.4: Performance-Based Failure Reporting, Analysis & Corrective Action System (FRACAS) Requirements
Abstract: This standard establishes uniform requirements and criteria for a performance-based Failure Reporting, Analysis & Corrective Action System (FRACAS). The performance-based aspect of this standard requires that the ...
AIAA SP-085: Fire, Explosion, Compatibility, and Safety Hazards of Hypergols - Monomethylhydrazine
Abstract: Monomethylhydrazine (MMH, CH3N2H3) is used as an aerospace fuel and an antioxidant in industrial processes and is used in the production of pesticides and pharmaceuticals. MMH is a strong ...
AIAA S-061: Commercial Launch Safety
Abstract: Space launch ground and flight activities by their nature create safety risks to personnel, public and private property and the environment. This standard identifies the safety roles and responsibilities for the conduct ...
AIAA G-034A: Guide to Reference and Standard Ionosphere Models
Abstract: This guide describes the content of the models, uncertainties and limitations, technical basis, databases from which the models are formed, publication references, and sources of computer codes for 46 ionospheric models ...
AIAA S-133-3: Space Plug-and-Play Architecture Standard Logical Interface
Abstract: The SPA logical interface is the conceptual boundary through which components are able to participate in a SPA system. Unlike a physical interface which defines connectors, pin-outs, and signaling levels, the logical ...
AIAA SP-084: Fire, Explosion, Compatibility, and Safety Hazards of Hypergols - Hydrazine
Abstract: Hydrazine is a colorless, corrosive, strongly reducing liquid compound. Current aerospace applications include its use in the Space Transportation System as a fuel for the auxiliary power units, in satellites as a ...
AIAA SP-086: Fire, Explosion, Compatibility, and Safety Hazards of Nitrogen Tetroxide
Abstract: Nitrogen tetroxide (NTO) is a corrosive, strongly oxidizing liquid compound used chiefly in aerospace propulsion and power systems. It is currently used in the Space Shuttle as an oxidizer for the Orbital Maneuvering System ...
AIAA S-117: Space Systems Verification Program and Management Process
Abstract: This standard establishes a set of requirements for planning and executing verification programs for both manned and unmanned space systems.
This standard enforces the distributed verification program among general ...
This standard enforces the distributed verification program among general ...
AIAA S-133-4: Space Plug-and-Play Architecture Standard Physical Interface
Abstract: Mechanical, thermal and electrical connector interface requirements are contained in this document. These requirements include details of the mounting hole pattern, fastener clearance-hole sizes, and thermal control ...
AIAA S-102.1.5: Performance-Based Failure Review Board (FRB) Requirements
Abstract: 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 ...