EA-WI-023 (REV. C), Project Management of GFE Flight Projects. This work instruction defines the project management processes and associated products for the definition, planning and implementation of GFE Flight Development Projects. These processes and products are defined in association with specific life cycle phases. For each phase, required prerequisites, processes, products, and control gates are documented. In addition, this work instruction defines project configuration management, project contract procedures, and templates for key products and forms.

JPG 5322.1 (REV. D), CONTAMINATION CONTROL REQUIREMENTS MANUAL (MAY 2000) [FORMERLY JSCM 5322]., The JSC Contamination Control Requirements Manual establishes the requirements and criteria for coordinated contamination control activities. This manual provides the minimum controls necessary to establish and maintain an effective contamination control system. JSCM 8080, "JSC Design and Procedural Standards Manual," stipulates additional mandatory contamination control requirements. The latest issue of JSCM 8080 should be reviewed to ensure that standards relating to contamination control which are issued after publication of this document are also implemented.

JPR 1700.1I, (JULY 2002), JSC SAFETY AND HEALTH HANDBOOK., Chapter 1.0 provides an overview of and basic requirements for JSC’s safety and health program. It also includes general information about who must follow this Handbook, and how to use it.

JPR 1710.13C, DESIGN, INSPECTION, AND CERTIFICATION OF PRESSURE VESSELS AND PRESSURIZED SYSTEMS (AUG 2004)., Presented in this document are requirements for design, inspection, and certification of ground-based pressure vessels and pressurized systems (PV/S) owned and/or operated by JSC and of all PV/S used on JSC property. JSC organizations must implement these requirements on PV/S for which they have the responsibility.

LS-20079-2A, EXPERIMENT DOCUMENT FORMAT AND INSTRUCTIONS FOR HUMAN LIFE SCIENCES FLIGHT RESEARCH EXPERIMENTS (SEP 2003)., This document establishes and controls requirements for PI activities, selection and training of flight crew members, integration and ground processing of flight experiment equipment, and collection,processing, and archiving of experiment data.

LS-71002, SYSTEM SAFETY PROGRAM PLAN (SSPP) FOR THE HUMAN RESEARCH FACILITY (AUG 1998)., Program system safety includes all HRF supplied hardware hazard identification,control, and verification during ground handling, shuttle flight, transfer to ISS, on orbit installation, operations and maintenance, and return to earth.

LS-71011A, ACOUSTIC NOISE CONTROL AND ANALYSIS PLAN FOR HUMAN RESEARCH FACILITY PAYLOADS AND RACKS (19 OCT 2001)., The Human Research Facility (HRF) is a facility class payload that consists of a suite of generic human life sciences hardware needed to support a multidisciplinary research program that encompasses basic, applied, and operations research. The HRF will include equipment to support research to understand the effects of weightlessness and the space environment on human systems and to develop, where appropriate, methods to counteract these effects to ensure safe and efficient crew operations. This document provides a general outline of the acoustic control plan and analysis approach. Section 2 describes the ISS acoustic design requirement. Section 3, introduces the general theory of sound propagation and analytical formulations to LS-71011 - 05/30/01 1-2 compute SPLs. Section 4 describes the acoustic analysis approach which will be used to perform the rack level, component level analysis process, and component level suballocation procedure. Section 5 investigates the methods of noise control. A summary is provided in Section 6. Appendix A describes the noise measurement procedures for ISS Government Furnished Equipment (GFE) equipment and payloads. This appendix was provided by JSC-SP3. The document, JSC-26218, Spacelab Life Sciences 2 Acoustic Analysis Report [21], is an example of a typical acoustics analysis involving several sources located in different locations in an enclosed volume operated intermittently or continuously according to a timeline. In case of conflicts between this document and LS-71000, HRF Program Requirements Document [22], LS-71000 takes precedence

LS-71020-1A, SOFTWARE CONFIGURATION MANAGEMENT PLAN AND PROCEDURE FOR THE HUMAN RESEARCH FACILITY, CCB CONTROLLED (11 JAN 2001)., The purpose of this document is to establish and maintain the integrity of the software products for the Human Research Facility (HRF). Software Configuration Management (SCM) involves: a) Identifying and cataloging the components and configurations of the HRF software (SW) b) Systematically controlling changes to the HRF SW configuration c) Maintaining the integrity and traceability of the HRF SW configuration(s) d) Auditing the HRF SW configuration e) Documenting and periodically reviewing the HRF SCM procedures The HRF SW placed under SCM includes all HRF SW delivered to the customer as well as applications software and related systems software, compilers, and firmware. SCM will be maintained throughout the HRF life-cycle.

LS-71020B, SOFTWARE DEVELOPMENT PLAN FOR THE HUMAN RESEARCH FACILITY, CCB CONTROLLED (JAN 2001), The Software Development Plan (SDP) for the Human Research Facility (HRF) establishes the programmatic requirements, policies, procedures and guidelines for software development, testing and sustaining engineering in addition to those requirements set forth in the Program Requirements Document (PRD) for the HRF (LS-71000). The following types of software will be either developed or acquired for the HRF to fulfill the Functional Requirements Document (FRD) for the HRF (LS-71001) and PRD specifications: a) Flight Software b) Ground Support Software (GSS) c) Test and Simulation Software This SDP establishes the policies, procedures and guidelines for development, testing and sustaining engineering of software developed for HRF experiments. The SDP document templates illustrate how requirements traceability from the Hardware Requirements Document (HRD) to the HRF Software Requirement and implementing computer software configuration item (CSCI) is managed. Configuration Management policies and procedures for HRF software are documented in the Software Configuration Management Plan and Procedures for the HRF (LS-71020-1).

LS-71042, HARDWARE DEVELOPMENT PLAN FOR THE WORKSTATION HUMAN RESEARCH FACILITY (JULY 1996)., The purpose of this document is to define the development plan of the Human Research Facility (HRF) Workstation. This document will outline the steps required to prototype, design, fabricate, test and certify the hardware, as well as define the major programmatic and developmental milestones in the project.

LS-71042-14-4B, INTERFACE DEFINITION DOCUMENT (IDD) FOR THE HUMAN RESEARCH FACILITY (HRF), RACK 2 WORKSTATION (R2WS) (22 OCT 2004)., This Interface Definition Document (IDD) describes: 1. The interfaces provided by the Human Research Facility (HRF) Rack 2 Workstation (R2WS) P/N: SEG46118400-302. 2. The interfaces between the HRF R2WS and the International Space Station (ISS) and the HRF Racks. The R2WS interfaces to be described include: Electrical, data, audio/video (A/V), mechanical, and thermal. No attempt has been made to define the human factors user or software (S/W) interfaces; those tasks are considered out of scope for this document.

LS-71062-8D, INTERFACE DESIGN DOCUMENT FOR THE HUMAN RESEARCH FACILITY COMMON SOFTWARE (10 OCT 2003)., This document describes the interfaces of the Human Research Facility (HRF) Common Software (CSW) required for payload client software connectivity. The CSW provides user and client software access to launching payload software and controlling telemetry of payload data to the ground by passing the corresponding data to the Rack Interface Controller (RIC). This document provides all information needed to generate an interface to the CSW.

LS-71130, HUMAN RESEARCH FACILITY (HRF) HUMAN-COMPUTER INTERFACE (HCI) DESIGN GUIDE (24 NOV 1997)., The Human-Computer Interface (HCI) Design Guide for the Human Research Facility HRF is intended as a brief, easy to use reference guide for the designers of all HCIs within the HRF, including the ground development facility. The approach of this document effort was to compile and summarize selected HCI guidelines collected from numerous published texts. This document should: (1) educate designers in the HCI design process and basic design principles, (2) point designers to additional resources where necessary and (3) be used to establish a common ground for collaboration with human factors professionals in the design of HRF HCIs. This document does not control the HRF software development and configuration management processes defined in the Software Development Plan for the Human Research Facility (LS-71020), however, the HCI design process described in this document should be integrated into the software development process by the user interface design team. This design guide is relevant to all software interfaces for HRF components, whether they be a portable or workstation computer, or any device that includes an electronic visual display. This guide should be referenced for all procurement activity where the vendor will write HRF specific software, but it is not applicable to Commercial-Off-the-Shelf (COTS) software and other software not specifically written for HRF. Given the potential for multiple software platforms within HRF, this document should be used in conjunction with platform specific HCI guidelines, such as those referenced in Section 7.0. Consultation and/or collaboration with human factors professionals is strongly recommended in order to ensure proper implementation of these guidelines.

NASA DC-8, AIRBORNE LABORATORY EXPERIMENTER HANDBOOK (JUN 2002). This aircraft, extensively modified as a flying laboratory, is based at Dryden Flight Research Center (DFRC), Edwards, California. It is operated for the benefit of researchers whose proposals have been previously approved by NASA Headquarters. Airborne laboratory flights may be operated out of DFRC or from deployment sites worldwide, according to the research requirements.

NASA SP-T-0023C, SPACE SHUTTLE SPECIFICATION ENVIRONMENTAL ACCEPTANCE TESTING. This Environmental Acceptance Test Specification establishes the minimum test and documentation requirements to be met by NASA and its contractors in the environmental acceptance testing of hardware, both Government-furnished and contractor-furnished, for use in SSP applications.

SL-E-001 (REV. D), SPACE SHUTTLE SPECIFICATION-ELECROMAGNETIC COMPATIBILITY REQUIREMENT (13 MAY 1998)., This specification has been prepared specifically to tailor the requirements of MIL-E-6051D, dated September 7, 1967, to the Space Shuttle Program and elements thereof. It is applicable to all NASA Space Shuttle System procurements at the project level or higher. All elements of the SSP must adhere to these baselined requirements.

SM3-WI-008, PAYLOAD AND EXPERIMENT REVIEWS (24 AUG 2001), Mission and Project Management Office, Biomedical Systems Test and Project Management Office. The Biomedical Systems Test and Project Management Office (SM3) conducts status reviews at various payload and experiment levels for investigations managed by SM3. The type of review and requirements of the review schedule is unique to the program and adheres to the program. This SM3 Work Instruction (WI) is a guide for the local implementation of payload and experiment reviews for life sciences experiments managed by SM3. The level of detail and schedule for the conduct of the reviews are program dependent. This WI is applicable to all NASA and contractor personnel who are associated with the design and development of SM3 managed life sciences experiments and payloads. This WI applies to both payload and experiment level reviews.

SN-C-0005D, SPACE SHUTTLE CONTAMINATION CONTROL REQUIREMENTS. This specification contains contamination control requirements applicable to space vehicles and Ground Support Equipment (GSE) from design concept through procurement, fabrication, assembly, test, storage, delivery, launch/ground operations, and maintenance for the SSP.