AIAA G 020 : 1992
Withdrawn
A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.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
23-07-2013
12-01-2013
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Withdrawn
|
| AIAA R 021 : 1992 | RECOMMENDED PRACTICE FOR SPACECRAFT SYSTEM DESIGN IN SI UNITS |
| AIAA R 020 : A1999 | RECOMMENDED PRACTICE FOR MASS PROPERTIES CONTROL FOR SATELLITES, MISSILES, AND LAUNCH VEHICLES |
| 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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