In June, Harmony Myers transitioned from serving as the System Safety Technical Discipline Team Lead to overseeing the NASA Safety Center (NSC) Technical Excellence Office (TEO). Myers is excited for her new role as director of TEO and already has plans on how to improve collaboration among the NSC’s four offices and across the agency.

NPR 8735.1 Revision D, Exchange of Problem Data Using NASA Advisories and the Government-Industry Data Exchange Program went into effect July 29, 2018. 

Your thoughts, comments and suggestions about the Safety Culture at NASA have been heard. The Office of Safety and Mission Assurance, along with Subject Matter Experts from each of the NASA centers, has worked to make changes throughout the agency based on your input from the NASA Safety Culture Survey.

Last December, Anthony “Tony” DiVenti stepped into a new role as the Office of Safety and Mission Assurance Reliability and Maintainability (R&M) technical fellow. DiVenti sought this position because of his passion for R&M and his desire to improve tools, methods and training and hopefully remove barriers that may prevent R&M professionals from performing their jobs in the most effective and efficient manner.

The most recent EEE Parts Bulletin provides information on activities related to Electrical, Electronic and Electromechanical (EEE) parts that occurred at NASA between August 2017 and May 2018. 

This summer, about 120 people from NASA, the European Space Agency and the Japan Aerospace Exploration Agency — and their contactor and assurance research communities — gathered at NASA Kennedy Space Center for the fifth Trilateral Safety and Mission Assurance Conference (TRISMAC). 

The Office of Safety and Mission Assurance (OSMA) created a new program dedicated to developing projects focused on moving demonstrations to best practices in the emerging Model-Based Systems Engineering (MBSE) paradigm. The Model-Based Mission Assurance (MBMA) Program will work to facilitate the integration of assurance functions and requirements into the project model. 

The four guiding principles in the U.S. Government Orbital Debris Mitigation Standard Practices, approved in 2001, are to limit the generation of mission-related debris, accidental explosions and collisions, and to conduct postmission disposal. Both the 2006 and 2010 U.S. National Space Policies directed U.S. government departments and agencies to implement the standard practices to limit the generation of new debris by their space missions. NPR 8715.6, NASA Procedural Requirements for Limiting Orbital Debris and Evaluating the Meteoroid and Orbital Debris Environments and NASA-STD-8719.14, Process for Limiting Orbital Debris represent the agency’s implementation of the standard practices.

Updates to American National Standards Institute (ANSI)/American Institute of Aeronautics and Astronautics (AIAA) S-080A, Space Systems—Metallic Pressure Vessels, Pressurized Structures, and Pressure Components and ANSI/AIAA S-081B, Space Systems—Composite Overwrapped Pressure Vessels went into effect March 2018. 

Recently, the Expendable Launch Vehicle (ELV) Payload Safety Program released a new course “Safety Guidance for Payloads” (SMA-HQ-WBT-104) to the agency in SATERN. The course focuses on ensuring a consistent level of safety for special-case ELV payloads, which are payloads that either 1) don’t use the Launch Services Program or 2) rideshare with a primary payload on an ELV.