SMC-T-004 (2012), AIR FORCE SPACE COMMAND (AFSC) SPACE AND MISSILE SYSTEMS CENTER - TAILORING: TAILORING INSTRUCTIONS FOR MIL-STD-882E (30-NOV-2012)

SMC-T-004 (2012), AIR FORCE SPACE COMMAND (AFSC) SPACE AND MISSILE SYSTEMS CENTER - TAILORING: TAILORING INSTRUCTIONS FOR MIL-STD-882E (30-NOV-2012)., The new-issue SMC tailoring adds some System Safety practices for Air Force Space and Missile Systems to MIL-STD-882E, while removing nothing. The tailoring is indented to assist the user in following pertinent requirements of policy implementation documents. For example, when define USAF preventable mishaps, include all reportable mishaps, which include losses of systems and their mission capability (particularly in space systems) in addition to other types of losses. This tailored standard applies to the entire life cycle of systems, which for space systems includes pre-launch, launch and on-orbit including disposal. Apply this tailoring in coordination with other functional areas taking advantage of the Systems Engineering process to ensure affordable robust systems. This document shall be used for tailoring MIL-STD-882E dated 11 May 2012, and provides a contractual Compliance Document listing that cites MIL-STD-882E and an annex with tailoring instructions. This document is intended for use in acquisition contracts for space systems and shall be cited in the contract Statement of Work (SOW) to specify the system safety requirements that are applicable to the acquisition of space systems or space system of systems (SoS) which may include space vehicles, upper-stage vehicles, injection stages, satellite payloads, reentry vehicles, launch vehicles or ballistic vehicles, ground control systems and user equipment systems.