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MSFC-HDBK-3051 REV A - MICROGRAVITY SCIENCE GLOVEBOX (MSG) CAPABILITIES MANUAL Organization: MSFC
Date: 2002-10-16
Description: The Microgravity Science Glovebox (MSG) is a double rack facility designed for microgravity investigation/experiment handling aboard the International Space Station (ISS).
MSFC-PLAN-2958 REV A CHG NOTICE 1 - PROJECT PLAN FOR MICROGRAVITY SCIENCE GLOVEBOX (MSG) Organization: MSFC
Date: 2004-12-14
Description: Introduction This Project Plan describes the top-level requirements and overall approach to be utilized by the Marshall Space Flight Center (MSFC) for the Microgravity Science Glovebox (MSG) Project on the International Space Station (ISS).
MSFC-PLAN-3052 REV C - MICROGRAVITY SCIENCE GLOVEBOX (MSG) INVESTIGATION INTEGRATION PLAN Organization: MSFC
Date: 2005-11-09
Description: PURPOSEThe purpose of this document is to define the Microgravity Science Glovebox (MSG) investigations integration process. The MSG LevelĀ III Configuration Control Board (CCB) controls this document per MSFC-PLAN-2781.
MSFC-PLAN-2781 REV C CHG NOTICE 3 - ED43 CONFIGURATION MANAGEMENT PLAN FOR MICROGRAVITY SCIENCE GLOVEBOX (MSG) Organization: MSFC
Date: 2005-03-02
Description: INTRODUCTION The Configuration Management Plan (CMP) defines requirements, responsibilities, and procedures for the Microgravity Science Glovebox (MSG) Facility and MSG Investigation Integration project activity.
MSFC-RQMT-2888 REV F - MICROGRAVITY SCIENCE GLOVEBOX (MSG) INVESTIGATION INTERFACE REQUIREMENTS DOCUMENT Organization: MSFC
Date: 2006-06-23
Description: This IIRD is the interface design requirements document for Microgravity Science Glovebox (MSG) Investigations.
MSFC-RQMT-3406 REV D - MICROGRAVITY SCIENCE GLOVEBOX (MSG) ANCILLARY HARDWARE REQUIREMENTS DOCUMENT Organization: MSFC
Date: 2006-03-16
Description: This document defines all Microgravity Science Glovebox (MSG) ancillary hardware requirements and verification requirements.
MSFC-RQMT-3218 REV F - MICROGRAVITY SCIENCE GLOVEBOX (MSG) ANCILLARY HARDWARE REQUIREMENTS VERIFICATION MATRIX Organization: MSFC
Date: 2006-03-16
Description: The purpose of this document is to define the complete set of verification activities necessary to ensure ancillary hardware compliance with the SSP 57411 V1, Microgravity Science Glovebox (MSG) Verification Plan Volume 1. The MSG ancillary hardware requirements verification matrix defines and controls ancillary hardware verification requirements to meet the International Space Station (ISS) Pressurized Payloads Interface Requirements Document, SSP 57000.
MSFC-RQMT-3163 REV B - GLOVEBOX INTEGRATED MICROGRAVITY ISOLATION TECHNOLOGY (G-LIMIT) INVESTIGATION INTERFACE REQUIREMENTS DOCUMENT Organization: MSFC
Date: 2003-02-04
Description: This Investigation Interface Requirements Document (IIRD) defines and controls required MSG Investigation interfaces for compatibility with the Glovebox Integrated Microgravity Isolation Technology (g-LIMIT).
MSFC-PLAN-3140 REV B CHG NOTICE 2 - MICROGRAVITY SCIENCE GLOVEBOX (MSG) FACILITY MANAGEMENT AND INVESTIGATION INTEGRATION SAFETY & MISSION ASSURANCE PLAN Organization: MSFC
Date: 2005-05-05
Description: This document was prepared by the Marshall Space Flight Center (MSFC) Cargo Assurance Department (QD30) to define Safety, Reliability, Maintainability and Quality Assurance activities performed by QD30 for the Microgravity Science Glovebox (MSG) facility managed by the MSFC Space Systems Program/Project Office (SSPPO).
MSFC-HDBK-3164 - GLOVEBOX INTEGRATED MICROGRAVITY ISOLATION TECHNOLOGY (G-LIMIT) CAPABILITIES HANDBOOK Organization: MSFC
Date: 2001-12-17
Description: The ISS, designed as a research laboratory, will utilize the near-zero acceleration environment of low-earth orbit for unique high-tech microgravity science investigations.
ASTM C852 - STANDARD GUIDE FOR DESIGN CRITERIA FOR PLUTONIUM GLOVEBOXES Organization: ASTM
Date: 2009-06-01
Description: This guide defines criteria for the design of glovebox systems to be used for the handling of plutonium in any chemical or physical form or isotopic composition or when mixed with other elements or compounds.
MSFC-HDBK-3256 - GLOVEBOX INTEGRATED MICROGRAVITY ISOLATION TECHNOLOGY (G-LIMIT) TELEMETRY DATA DISPLAYS UTILIZING PAYLOADS AND COMPONENTS REAL-TIME AUTOMATED TEST SYSTEM (PACRATS) USER GUIDE Organization: MSFC
Date: 2002-04-15
Description: PACRATS has the capability to display integer and float values with a digital meter, graphs with multiple or single plots, or tables with multiple values. PACRATS was designed to: Provide a generic data acquisition system for test personnel.
SAE/TP - 2009-01-2468 - SMOKE PARTICLE SIZES IN LOW-GRAVITY AND IMPLICATIONS FOR SPACECRAFT SMOKE DETECTOR DESIGN Organization: SAE/TP
Date: 2009-07-12
Description: This paper presents results from a smoke detection experiment entitled Smoke Aerosol Measurement Experiment (SAME) which was conducted in the Microgravity Science Glovebox on the International Space Station (ISS) during Expedition 15.
ASTM C1572 - STANDARD GUIDE FOR DRY LEAD GLASS AND OIL-FILLED LEAD GLASS RADIATION SHIELDING WINDOW COMPONENTS FOR REMOTELY OPERATED FACILITIES Organization: ASTM
Date: 2010-11-01
Description: This standard is intended to be generic and to apply to a wide range of configurations and types of lead glass radiation shielding window components used in hot cells. It does not address glovebox, water, x-ray glass or zinc bromide windows. Supplementary information on viewing systems in hot cells may be found in Guides C1533 and C1661.

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