درباره ما
AIAA - American Institute of Aeronautics and Astronautics: Recent submissions
Now showing items 21-40 of 70
-
AIAA G-083
Abstract: Introduction
Increasing concerns over trapped radiation effects on microelectronics, coupled with the availability of new data, long-term changes in the Earth's magnetic field, and variations in the ... -
AIAA S-081A
Abstract: This standard establishes baseline requirements for the design, fabrication, test, inspection, operation and maintenance of composite overwrapped pressure vessels (COPVs) containing a metallic liner. These vessels are used ... -
AIAA S-112A
Abstract: This document establishes qualification and quality requirements for the electrical components integrated onto spacecraft solar panels that carry single crystal silicon solar cells or gallium arsenide solar cells having ... -
AIAA S-115
Abstract: This document and information handbook presents an overview of the current understanding of the various plasma interactions that can result when a high-voltage system is operated in the Earth's ionosphere. This document ... -
AIAA G-118
Abstract: The purpose of this Guide is to assist development and maintenance projects (teams and individuals) that have to address the use of, or consideration of, COTS products within large, complex systems, including but not limited ... -
AIAA S-114
Abstract: This standard specifies general requirements for the design, manufacture, quality control, testing, and storage of moving mechanical assemblies (MMAs) to be used on space and launch vehicles. This standard is applicable ... -
AIAA G-077
Abstract: The fundamental strategy of V&V is the assessment of error and uncertainty in the computational simulation. The required methodology is a complex process because it must assess errors and uncertainties originating in all ... -
AIAA S-133-9
Abstract: This document specifies the means by which the SPA features of networked component registration and message routing to endpoints on a SpaceWire network are facilitated. Accomplishing this requires lowlevel messaging on the ... -
AIAA S-102.2.18
Abstract: This standard establishes uniform requirements and criteria for a performance-based fault tree analysis (FTA), including the modeling components, symbols, and analytical objectives. The performance-based aspect of this ... -
AIAA G-003C
Abstract: This standard provides guidelines for selected reference and standard atmospheric models for use in engineering design or scientific research. The guide describes the content of the models, uncertainties and limitations, ... -
AIAA S-121
Abstract: This standard is applicable for the procurement of space systems, including spacecraft, space vehicles, launch vehicles, ground systems, and associated equipment/subsystems.
This standard establishes performance and ... -
AIAA G-133-1
Abstract: This Guidebook provides an overview for spacecraft platform (system), subsystem, and component (including payload) developers with spacecraft plug-and-play architectures to promote rapid design, fabrication, integration, ... -
AIAA S-071A
Abstract: Introduction
Wind tunnel data are often presented without reference to the quality of the results. When data uncertainty is considered, it is normally in the form of repeatability from a few supposedly ... -
AIAA G-072
Abstract: This guide provides historical information for three classes of utility connectors, manual, robotic, and automated for use on aircraft and space vehicles. Applications include ground and on-orbit servicing of spacecraft, ... -
AIAA S-133-8
Abstract: This document provides detail for incorporation of Test Bypass (TB) functionality in SPA components and systems, and describes the messaging protocol for TB. Test Bypass is the mechanism by which test data may be injected ... -
AIAA S-102.2.11
Abstract: This standard establishes uniform requirements and criteria for a performance-based anomaly detection and response (ADR) analysis process. The performance-based aspect of this standard requires that the organizationʼs ... -
AIAA R-092-1
Abstract: Introduction
Wind tunnel testing is a critical component in the development of aerodynamic vehicles and associated technologies. While the time and expense of wind tunnel testing is significant, it is ... -
AIAA G-140
Abstract: This AIAA Guide provides guidelines regarding the current natural terrestrial environment criteria for use in the design and development of aerospace vehicles traversing the terrestrial atmosphere (0–90 km altitude). ...