Name | Support | Language | Availability | Edition date | Price | ||
---|---|---|---|---|---|---|---|
PDF |
English |
Active |
10/14/2015 |
€80.00 |
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Details
AIAA S-120A-2015 defines terminology and establishes uniform processes, procedures, and methods for the
management, control, monitoring, determination, verification, and documentation of mass properties
during the design and development phases of space systems, including modifications to operational
systems. This standard applies to space vehicles (SVs) or spacecraft (SC), upper stage vehicles, injection
stages, satellite payloads, reentry vehicles, launch vehicles (LVs), and ballistic vehicles. This standard
defines a minimum set of mass properties requirements and is intended for use in developing a programspecific,
contractually required mass properties control plan (MPCP). When used in conjunction with the
International Society of Allied Weight Engineers, Inc. (SAWE) Recommended Practice RP A-3, the two
documents serve as a comprehensive reference for requirements and best practices in the field of space
systems mass properties.
Additional Info
Author | American Institute of Aeronautics and Astronautics |
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Published by | AIAA |
Document type | Standard |
EAN ISBN | 9781624103858 |
Number of pages | 39 |
Replace | AIAA S-120-2006 |
Keyword | AIAA S-120A-2015 |
ANSI Approved |