Now showing items 41-60 of 70

    • AIAA R-060 

      Type: standard
      Source: AIAA - American Institute of Aeronautics and Astronautics:;1993
      Organization : AIAA - American Institute of Aeronautics and Astronautics
      Abstract: Definitions and terms used in vehicle performance comparisons are specified. Orbital profiles are specified for generating comparison missions (e.g., 185 km circular orbit from Cape Canaveral). A table of current launch ...
    • AIAA S-110 

      Type: standard
      Source: AIAA - American Institute of Aeronautics and Astronautics:;2005
      Organization : AIAA - American Institute of Aeronautics and Astronautics
      Abstract: This document establishes a standard for the design, analysis, material selection and characterization, fabrication, test, and inspection of structural items in space systems, including payloads, spacecraft, upper-stages, ...
    • AIAA S-133-7 

      Type: standard
      Source: AIAA - American Institute of Aeronautics and Astronautics:;2013
      Organization : AIAA - American Institute of Aeronautics and Astronautics
      Abstract: Two functions are critical in defining an ontology: Naming conventions and relationships between the names. The naming conventions have been selected to cover the complete domain of data elements and characteristics to be ...
    • AIAA S-102.2.5 

      Type: standard
      Source: AIAA - American Institute of Aeronautics and Astronautics:;2009
      Organization : AIAA - American Institute of Aeronautics and Astronautics
      Abstract: This standard establishes uniform requirements and criteria for a performance-based sneak circuit analysis (SCA). This performance-based aspect of this standard requires that the organization's SCA capability be rated ...
    • AIAA SP-016-2 

      Type: standard
      Source: AIAA - American Institute of Aeronautics and Astronautics:;1999
      Organization : AIAA - American Institute of Aeronautics and Astronautics
    • AIAA R-099 

      Type: standard
      Source: AIAA - American Institute of Aeronautics and Astronautics:;2001
      Organization : AIAA - American Institute of Aeronautics and Astronautics
      Abstract: Introduction
      General
      Critical to establishing the required scope of space launch integration (SLI) for a spacecraft (SC) program is fully understanding the complexity and criticality ...
    • AIAA R-020A 

      Type: standard
      Source: AIAA - American Institute of Aeronautics and Astronautics:;1999
      Organization : AIAA - American Institute of Aeronautics and Astronautics
      Abstract: The management and control of mass properties is of fundamental importance in the design and manufacturing process of aerospace hardware. Mass properties are to be managed and controlled as any other system performance ...
    • AIAA S-111A 

      Type: standard
      Source: AIAA - American Institute of Aeronautics and Astronautics:;2014
      Organization : AIAA - American Institute of Aeronautics and Astronautics
      Abstract: This document establishes qualification and quality requirements for crystalline silicon and gallium arsenide-based single and multiple junction solar cell types for space applications. This includes requirements for solar ...
    • AIAA G-056 

      Type: standard
      Source: AIAA - American Institute of Aeronautics and Astronautics:;1992
      Organization : AIAA - American Institute of Aeronautics and Astronautics
      Abstract: Purpose
      The purpose of this document is to provide design guidelines for mechanical berthing / docking interface between space structures, elements, and serviceable or servicer vehicles. Intended ...
    • AIAA G-010 

      Type: standard
      Source: AIAA - American Institute of Aeronautics and Astronautics:;1993
      Organization : AIAA - American Institute of Aeronautics and Astronautics
      Abstract: This Guide commences with a discussion of domain analysis, followed by component assessment and concludes with the role of a reuse library. Section 2.0 defines domain analysis, and describes the principal products of such ...
    • AIAA S-080 

      Type: standard
      Source: AIAA - American Institute of Aeronautics and Astronautics:;1998
      Organization : AIAA - American Institute of Aeronautics and Astronautics
      Abstract: Purpose
      This standard establishes baseline requirements for the design, fabrication, test, inspection, operation and maintenance of the metallic pressurized hardware used in space systems such as ...
    • AIAA SP-016 

      Type: standard
      Source: AIAA - American Institute of Aeronautics and Astronautics:;1992
      Organization : AIAA - American Institute of Aeronautics and Astronautics
    • AIAA R-091 

      Type: standard
      Source: AIAA - American Institute of Aeronautics and Astronautics:;2003
      Organization : AIAA - American Institute of Aeronautics and Astronautics
      Abstract: This document provides a recommended method for calibration of internal strain-gage balances used in wind tunnel testing. The practices include terminology, axis system definition, balance calibration methods, matrix, and ...
    • AIAA S-124 

      Type: standard
      Source: AIAA - American Institute of Aeronautics and Astronautics:;2007
      Organization : AIAA - American Institute of Aeronautics and Astronautics
    • AIAA S-133-6 

      Type: standard
      Source: AIAA - American Institute of Aeronautics and Astronautics:;2013
      Organization : AIAA - American Institute of Aeronautics and Astronautics
      Abstract: This standard is applicable to systems operating under the Space Plug-and-Play Architecture (SPA).
      The SPA System Timing Standard establishes a common method for providing common timing within a system of networked SPA ...
    • AIAA S-102.2.4 

      Type: standard
      Source: AIAA - American Institute of Aeronautics and Astronautics:;2009
      Organization : AIAA - American Institute of Aeronautics and Astronautics
      Abstract: This standard establishes uniform requirements and criteria for a performance-based, product Failure Mode, Effects and Criticality Analysis (FMECA). The performance-based aspect of this standard requires that the ...
    • AIAA G-133-10 

      Type: standard
      Source: AIAA - American Institute of Aeronautics and Astronautics:;2013
      Organization : AIAA - American Institute of Aeronautics and Astronautics
      Abstract: This document defines what constitutes a SPA system by outlining the basic principles of the architecture and the services that a SPA system provides. The capabilities defined herein flow-down to the individual SPA Standards ...
    • AIAA S-120 

      Type: standard
      Source: AIAA - American Institute of Aeronautics and Astronautics:;2006
      Organization : AIAA - American Institute of Aeronautics and Astronautics
      Abstract: This standard defines terminology and establishes uniform processes, procedures, and systematic methods for the management, control, monitoring, determination, verification, and documentation of mass properties during the ...
    • AIAA G-035A 

      Type: standard
      Source: AIAA - American Institute of Aeronautics and Astronautics:;2000
      Organization : AIAA - American Institute of Aeronautics and Astronautics
      Abstract: This Guide suggests methods for measuring human performance for scientific research and system test and evaluation. The information contained in this document is provided as guidance, not mandated as direction. This Guide ...
    • AIAA S-123 

      Type: standard
      Source: AIAA - American Institute of Aeronautics and Astronautics:;2007
      Organization : AIAA - American Institute of Aeronautics and Astronautics