MSFC-STD-100, CASTINGS, ALUMINUM AND MAGNESIUM ALLOY, RADIOGRAPHIC INSPECTION OF, ACCEPTANCE STANDARD FOR. This standard establishes acceptance standards for aluminum nad magnesium sand and permanent mold castings by the radiographic inspection method.

MSFC-STD-1249, STANDARD NDE GUIDELINES AND REQUIREMENTS FOR FRACTURE CONTROL PROGRAMS. This standard provides guidelines for selection and prescription of Non-Destructive Evaluation (NDE) techniques required to fulfill the demands of a Fracture Control program.

MSFC-STD-156, RIVETING, FABRICATION AND INSPECTION, STANDARD FOR (2 APR 1962)., This standard establishes the requirements for fabrication and inspection of rivets and fasteners and the procedures for riveting operations.

MSFC-STD-1800A, ELECTROSTATIC DISCHARGE (ESD) CONTROL FOR PROPELLANT AND EXPLOSIVE DEVICES (20 DEC 2004)., The purpose of this document is to establish requirements for the development of appropriate control measures to provide protection against personnel injury, property damage, and/or mission degradation due to the discharge of electrostatic energy (ESE) and subsequent initiation of propellant or explosive devices (ordnance).

MSFC-STD-246C, STANDARD DESIGN AND OPERATIONAL CRITERIA FOR CONTROLLED ENVIRONMENTAL AREAS. The purpose of this Standard is to present data and information that relate to contamination control of MSFC environmentally controlled areas, clean rooms, and flow benches. It specifies environmental control operating standards to be used as minimum criteria for rooms and hardware requiring environmental control. This Standard lists guidelines for selecting environmental facilities and for achieving the operating conditions necessary to achieve contamination control of critical aerospace hardware during MSFC operations; it also lists quality control measures to assure compliance.

MSFC-STD-2594C, MSFC FASTENER MANAGEMENT & CONTROL PRACTICES (1 MAY 2002)., This standard documents fastener management and control policy, responsibilities, and practices for structural fasteners, fracture critical fasteners, and safety critical fasteners (as defined by the program/project) that are procured, received, tested, inventoried or installed for space flight by George C. Marshall Space Flight Center (MSFC) or its contractors.

MSFC-STD-2806B, MSFC TAILORING GUIDE FOR THE GLOBAL DRAWING REQUIREMENTS MANUAL (GDRM) NINTH EDITION. This tailoring standard has been generated to document the exceptions to the use of the Global Drawing Requirements Manual (GDRM) within MSFC. The design organizations committee, which selected the GDRM, also prepared a listing of recommended exceptions that have been included in Section 4.0 of this standard. Revision A adds the requirement for preparation of an Engineering Order Graphics Data format and cancels the use of MSFC Form 421-1. This will facilitate use of design databases to generate the graphics information. In addition, the Appendix has been deleted and appropriate references have been added in the document to use the websites for selection of Applicable Documents for design requirements definition. In addition, the RCAR 177 team findings regarding Matched Set parts/assemblies have been incorporated. Revision B incorporates the GDRM 10th Edition to replace MIL-STD-100 in the MSFC requirements with ASME Y14.100-2000. This revision also states that if there is a conflict between the GDRM interpretation and ASME Y14.100-2000 requirements, the ASME Y14.100-2000 requirements take precedence.

MSFC-STD-2903B, MSFC TAILORING GUIDE FOR NASA-STD-8739.3, SOLDERED ELECTRICAL CONNECTION. This tailoring guide sets forth the Marshall Space Flight Center (MSFC) exceptions to the use of NASA-STD-8739.3, Soldered Electrical Connections, December 1997. This tailoring guide was prepared jointly by the Safety, Reliability & Quality Assurance (SR&QA) Policy and Assessment Department and the Electrical, Electronic, and Electromechanical (EEE) Parts, Packaging & Assembly Branch of the Instrument & Payload Systems Department. This guide shall be used on contracts and for in-house work.

MSFC-STD-2904, MSFC TAILORING GUIDE FOR NASA-STD-8739.2, WORKMANSHIP STANDARD FOR SURFACE MOUNT TECHNOLOGY. This tailoring guide sets forth the Marshall Space Flight Center (MSFC) exceptions to the use of NASA-STD-8739.2, Workmanship Standard for Surface Mount Technology, dated August 31, 1999. This tailoring guide was prepared jointly by the Safety, Reliability & Quality Assurance (SR & QA) Policy and Assessment Department and the Electrical, Electronic, and Electromechanical (EEE) Parts, Packaging & Assembly Branch of the Instrument & Payload System Department. This guide shall be used on contracts and for in-house work.

MSFC-STD-2905C, MSFC TAILORING GUIDE FOR NASA-STD-8739.4 CRIMPING INTERCONNECTING CABLES HARNESS AND WIRING. This tailoring guide sets forth the Marshall Space Flight Center (MSFC) exceptions to the use of NASA-STD-8739.4, Crimping, Interconnecting Cables, Harness, and Wiring, dated February 1998. This tailoring guide was prepared jointly by the Safety, Reliability & Quality Assurance (SR & QA) Policy and Assessment Department and the Electrical, Electronic, and Electromechanical (EEE) Parts, Packaging & Assembly Branch of the Instrument & Payload System Department. This guide shall be used on contracts and for in-house work.

MSFC-STD-2906C, MSFC TAILORING GUIDE FOR NASA-STD-8739.1, WORKMANSHIP STANDARD FOR STAKING AND CONFORMAL COATING OF PRINTED WIRING BOARDS AND ELECTRONIC ASSEMBLIES. This tailoring guide sets forth the Marshall Space Flight Center (MSFC) exceptions to the use of MSFC Tailoring Guide for NASA-STD-8739.1, Workmanship Standard for Staking and Conformal Coating of Printed Wiring Boards and Electronic Assemblies, dated August 1999. This tailoring guide was prepared jointly by the Safety, Reliability & Quality Assurance (SR & QA) Policy and Assessment Department and the Electrical, Electronic, and Electromechanical (EEE) Parts, Packaging and Assembly Branch of the Instrument and Payload System Department. This guide shall be used on contracts and for in-house work.

MSFC-STD-2906C, MSFC TAILORING GUIDE FOR NASA-STD-8739.1, WORKMANSHIP STANDARD FOR STAKING AND CONFORMAL COATING OF PRINTED WIRING BOARDS AND ELECTRONIC ASSEMBLIES. This tailoring guide sets forth the Marshall Space Flight Center (MSFC) exceptions to the use of MSFC Tailoring Guide for NASA-STD-8739.1, Workmanship Standard for Staking and Conformal Coating of Printed Wiring Boards and Electronic Assemblies, dated August 1999. This tailoring guide was prepared jointly by the Safety, Reliability & Quality Assurance (SR & QA) Policy and Assessment Department and the Electrical, Electronic, and Electromechanical (EEE) Parts, Packaging & Assembly Branch of the Instrument & Payload System Department. This guide shall be used on contracts and for in-house work.

This standard sets forth requirements for rigid printed wiring boards (PWB’s). The parts in conformance with this standard are intended for use in aircraft, spacecraft, launch vehicles, and mission-essential support equipment. These requirements shall be invoked by drawings and specifications for flight hardware and critical support equipment.

This Standard establishes a uniform set of requirements for electrical, electronic, and electromechanical (EEE) parts selection, management, and control for space flight and mission essential ground support equipment for Marshall Space Flight Center (MSFC) programs. The parts requirements described in this document are to be selectively applied based on equipment grade and mission needs as specified in the Project Specification. Individual equipment needs should be evaluated to determine the extent to which each requirement should be applied

MSFC-STD-3029 is the result of the reclassification and review of MSFC-SPEC-522B ("Design Criteria for Controlling Stress Corrosion Cracking") which was originated more than 25 years agao as a tool to control stress corrosion cracking throughout NASA programs.

MSFC-STD-3394A, STANDARD FOR CONTRACTOR CONFIGURATION MANAGEMENT FOR MSFC PROGRAMS/PROJECTS. This standard defines configuration management principles for design, development, integration, operation, and logistical support of Configuration Items and Computer Software Configuration Items managed by MSFC throughout the acquisition life cycle. It incorporates the industry-Government consensus standard ANSI-EIA 649 principles. The focus of this standard is on performance requirements rather than the details of the design solution. MSFC management of the CM process is based on insight of contractor practice and application of ANSI-EIA 649 principles. These principles are relevant to configuration management practices through the entire life cycle, including "technology" programs where technology is the precursor to product development. This standard applies only to the extent specified in contracts. An important function of this standard is to facilitate the use of automation tools by providing standard criteria of the CM process. The predominant media for exchange of information has transitioned from a paper base to a digital one. Information technology concepts and standards for data access, data transfer, and data sharing have increased the opportunity for Government and industry to productively integrate information from distributed sources. This leads to a true virtual enterprise that includes all the Configuration Management information necessary for the life cycle support and maintenance of equipment and software.

MSFC-STD-3425, DESIGN STANDARDS FOR RIGID PRINTED CIRCUIT BOARDS AND ASSEMBLIES, This process standard establishes Marshall Space Flight Center (MSFC) exceptions to the use of the IPC-2221A and IPC-2222 requirements for the design of rigid printed boards and assemblies. This standard is intended for use on contracts and for in-house work.

MSFC-STD-3459, QUALITY PROGRAM PROVISIONS FOR MSFC TEST AREA CONTRACTORS. This publication establishes tailored general and specific requirements for quality assurance programs for the MSFC Test Area activities. Requirements of this publication should be invoked contractually to the extent needed, and consistent with program, project and contract requirements. This document supercedes MSFC-HDBK- 1630 Rev. A, and was changed to MSFC-STD-3459 to comply with current documentation rules. This publication meets the necessary requirements of SAE AS 9100, “Quality Systems-Aerospace-Model for Quality Assurance in Design, Development, Production, Installation and Servicing.” It is designed to provide requirements which address quality assurance programs for MSFC Test Area modification, buildup, activation, and operations.

MSFC-STD-366B, STANDARD PENETRANT INSPECTION METHOD. This specification has been approved by MSFC and is mandatory for use by MSFC and associated contractors.

MSFC-STD-372B, SILK SCREENING OF ELECTRICAL EQUIPMENT. This document establishes the requirements for silk screening of electrical equipment.

MSFC-STD-373A, LETTERING OF ELECTRICAL EQUIPMENT. This standard establishes the criteria for lettering of electrical equipment.

MSFC-STD-383E, STANDARD FOR RUBBER STAMPING OF ELECTRICAL EQUIPMENT AND COMPONENTS. This standard establishes the criteria for rubber stamping of electrical equipment and components.

MSFC-STD-397 (AMENDMENT 2), MFSC-NASA STANDARD RADIOGRAPHIC LABORATORY QUALIFICATION. This standard establishes the requirements for equipment, techniques, quality levels, reports, and records for qualified radiographic laboratories performing inspection of materials and parts intended for use in space vehicles and related structures.

MSFC-STD-481, STANDARD RADIOGRAPHIC INSPECTION AND ACCEPTANCE STANDARDS FOR FUSION-WELDED JOINTS IN STAINLESS AND HEAT-RESISTANT STEEL. This standard establishes the radiographic inspection adn acceptance standards for fusion welded joints in stainless and heat-resistant steel.

MSFC-STD-486B, STANDARD, THREADED FASTENERS, TORQUE LIMITS FOR (NOV 1992)., This standard sets the acceptable torque values for threaded fasteners used in space vehicles and support equipment, the methodology for establishing the torque limits for the same, ad criteria for torque indicating devices on such fasteners.

MSFC-STD-506C, STANDARD MATERIALS AND PROCESSES CONTROL. The purpose of this document is to define the minimum requiremetns for materials and processes for incorporation in spaceflight hardware procurements, technical programs, and designated ground support equipment.

MSFC-STD-509, MSFC/NASA STANDARD LUBRICANT SELECTION. This standard presents requirements applicable to the selection of lubricants for use in space vehicles and ground support equipment.

MSFC-STD-531, HIGH VOLTAGE DESIGN CRITERIA. This document was prepared...as a design/test guideline docment for [personnel] concerned with high voltage equipment and experiments...

MSFC-STD-555G, MSFC ENGINEERING DOCUMENTATION STANDARD. This document specifies the requirements and instructions for releasing Marshall Space Flight Center (MSFC) configuration documentation as specified in MWI 7120.4. It also specifies the requirements for preparing engineering drawings and parts lists. This standard is intended for MSFC in-house use only.

MSFC-STD-557A, STANDARD, THREADED FASTENERS, 6A1-4V TITANIUM ALLOY, USAGE CRITERIA FOR SPACECRAFT APPLICATIONS. This standard establishes criteria for use of 6Al-4V titanium alloy threaded fastener systems for spacecraft and associated equipment. These criteria are applicable to items designed and fabricated by MSFC and its prime contractors for use on MFSC programs.

MSFC-STD-561B, THREADED FASTENERS, REQUIREMENTS FOR SECURING OF FLIGHT HARDWARE USED ON SHUTTLE PAYLOADS AND EXPERIMENTS. This standard applies to Shuttle payloads (experiments, Mission Peculiar Equipment, etc.) for which MSFC has integration and or development responsibility. All structural and mechanical system hardware fasteners (NHB 1700.7) event.

MSFC-STD-781A, STANDARD FOR ELECTRICAL CONTACTS, RETENTION CRITERIA (1 AUG 2007)., The purpose of this document is to provide criteria for retention testing of electrical crimp, insertable/removable contacts. This document provides criteria for retention testing of contacts in electrical connectors and distribution/bussing junction devices conforming to specifications 40M38277, 40M38294, 40M38298, 40M39569, 40M39589, 16A02980, and MIL-DTL-38999. This criteria shall also be used for similar generic devices covered by industry, military, and other NASA specifications. This criteria does not apply to coaxial, shielded, or twist pin contacts.