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AIAA G 020 : 1992

Withdrawn

Withdrawn

A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.

GUIDE FOR ESTIMATING AND BUDGETING WEIGHT AND POWER CONTINGENCIES FOR SPACECRAFT SYSTEMS

Withdrawn date

07-23-2013

Published date

01-12-2013

Provides minimum weight and electrical power contingency requirements for the development and design of all spacecraft, systems, subsystems, components, and parts. It provides a detailed description of the stages of development and classes of design maturity. Contains provisions for the control of design parameters during each stage for each of four categories of weight or power.

DocumentType
Standard
PublisherName
American Institute of Aeronautics & Astronautics
Status
Withdrawn

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NASA MSFC HDBK 3173 : 2012 PROJECT MANAGEMENT AND SYSTEM ENGINEERING HANDBOOK
AIAA G 056 : 1992 Guide: Guide to the Serviceable Spacecraft Grasping/Berthing/Docking Interfaces<br>

AIAA R 020 : A1999 RECOMMENDED PRACTICE FOR MASS PROPERTIES CONTROL FOR SATELLITES, MISSILES, AND LAUNCH VEHICLES
AIAA R 060 : 1993 RECOMMENDED PRACTICE FOR REPORTING EARTH-TO-ORBIT MISSION PROFILES
AIAA G 056 : 1992 Guide: Guide to the Serviceable Spacecraft Grasping/Berthing/Docking Interfaces<br>
AIAA R 021 : 1992 RECOMMENDED PRACTICE FOR SPACECRAFT SYSTEM DESIGN IN SI UNITS

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