SMC-T-002
TAILORING INSTRUCTIONS FOR AIAA-S-120-2006
Year: 2008
Abstract: Purpose
This document shall be used for tailoring the AIAA Standard, S-120-2006 dated 1 December 2006, to provide effective program execution and mission success.
Application
This document is intended for use in acquisition and study contracts for space systems, and shall be cited in the contract statement of work to specify the mass properties control requirements that are applicable to the acquisition. The AIAA Standard Tailored by this technical operating report (TOR) (hereafter referred to as the "Tailored AIAA Standard") supersedes all revisions of MIL-STD-1811, MIL-HDBK-1811, MIL-M-38310, and TOR-2005(8583)-3970. The AIAA Standard approved on 1 December 2006 shall be tailored by this document as an effective baseline.
The tailored AIAA Standard shall also be used as a compliance document to specify mass properties control requirements for space vehicles, upper-stage vehicles, injection stages, satellite payloads, reentry vehicles, launch vehicles, or ballistic vehicles. When this standard is used as a reference document for these applications, the term "space systems" is to be interpreted as the applicable vehicle.
This document shall be used for tailoring the AIAA Standard, S-120-2006 dated 1 December 2006, to provide effective program execution and mission success.
Application
This document is intended for use in acquisition and study contracts for space systems, and shall be cited in the contract statement of work to specify the mass properties control requirements that are applicable to the acquisition. The AIAA Standard Tailored by this technical operating report (TOR) (hereafter referred to as the "Tailored AIAA Standard") supersedes all revisions of MIL-STD-1811, MIL-HDBK-1811, MIL-M-38310, and TOR-2005(8583)-3970. The AIAA Standard approved on 1 December 2006 shall be tailored by this document as an effective baseline.
The tailored AIAA Standard shall also be used as a compliance document to specify mass properties control requirements for space vehicles, upper-stage vehicles, injection stages, satellite payloads, reentry vehicles, launch vehicles, or ballistic vehicles. When this standard is used as a reference document for these applications, the term "space systems" is to be interpreted as the applicable vehicle.
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contributor author | AIR FORCE - 02 - Air Force Network Integration Center (AFNIC) | |
date accessioned | 2017-09-04T15:43:28Z | |
date available | 2017-09-04T15:43:28Z | |
date copyright | 08/08/2008 | |
date issued | 2008 | |
identifier other | PMDQJEAAAAAAAAAA.pdf | |
identifier uri | http://yse.yabesh.ir/std/handle/yse/45736 | |
description abstract | Purpose This document shall be used for tailoring the AIAA Standard, S-120-2006 dated 1 December 2006, to provide effective program execution and mission success. Application This document is intended for use in acquisition and study contracts for space systems, and shall be cited in the contract statement of work to specify the mass properties control requirements that are applicable to the acquisition. The AIAA Standard Tailored by this technical operating report (TOR) (hereafter referred to as the "Tailored AIAA Standard") supersedes all revisions of MIL-STD-1811, MIL-HDBK-1811, MIL-M-38310, and TOR-2005(8583)-3970. The AIAA Standard approved on 1 December 2006 shall be tailored by this document as an effective baseline. The tailored AIAA Standard shall also be used as a compliance document to specify mass properties control requirements for space vehicles, upper-stage vehicles, injection stages, satellite payloads, reentry vehicles, launch vehicles, or ballistic vehicles. When this standard is used as a reference document for these applications, the term "space systems" is to be interpreted as the applicable vehicle. | |
language | English | |
title | SMC-T-002 | num |
title | TAILORING INSTRUCTIONS FOR AIAA-S-120-2006 | en |
type | standard | |
page | 41 | |
status | Active | |
tree | AIR FORCE - 02 - Air Force Network Integration Center (AFNIC):;2008 | |
contenttype | fulltext |