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NASA - NSTS-ISS PUBS
NSTS 08307A, SPACE SHUTTLE CRITERIA FOR PRELOADED BOLTS
NSTS 08307A, SPACE SHUTTLE CRITERIA FOR PRELOADED BOLTS. The methodology and criteria defined in this document shall be applicable when it is determined that a bolted joint requires preloading to successfully perform its function. Generally, bolts that experience increased axial tensile loads as a result of the applied external load will require preloading to reduce cyclic stresses, prevent pressure leakage, prevent joint separation, or increase system stiffness. This methodology and criteria provides a set of minimum requirements which are adequate, but not overly conservative, so that the design and analysis of preloaded joints are addressed in a consistent and acceptable manner throughout the Space Shuttle Program.
Ident. Num:
NSTS 08307
Rev. Num:
A
NSTS 08307A, SPACE SHUTTLE CRITERIA FOR PRELOADED BOLTS. The methodology and criteria defined in this document shall be applicable when it is determined that a bolted joint requires preloading to successfully perform its function. Generally, bolts that experience increased axial tensile loads as a result of the applied external load will require preloading to reduce cyclic stresses, prevent pressure leakage, prevent joint separation, or increase system stiffness. This methodology and criteria provides a set of minimum requirements which are adequate, but not overly conservative, so that the design and analysis of preloaded joints are addressed in a consistent and acceptable manner throughout the Space Shuttle Program.
NSTS 1700.7B (ISS ADDENDUM)SAFETY POLICY AND REQUIREMENTS FOR PAYLOADS USING THE SPACE TRANSPORTATION SYSTEM (DEC 1995)
NSTS 1700.7B (ISS ADDENDUM)SAFETY POLICY AND REQUIREMENTS FOR PAYLOADS USING THE SPACE TRANSPORTATION SYSTEM (DEC 1995). This addendum to NSTS 1700.7B has been prepared to expand and modify the existing NSTS 1700.7B requirements such that International Space Station (ISS) payload safety requirements are identified to the ISS payload development organizations.
Ident. Num:
NSTS 1700.7
Rev. Num:
B
NSTS 1700.7B (ISS ADDENDUM)SAFETY POLICY AND REQUIREMENTS FOR PAYLOADS USING THE SPACE TRANSPORTATION SYSTEM (DEC 1995). This addendum to NSTS 1700.7B has been prepared to expand and modify the existing NSTS 1700.7B requirements such that International Space Station (ISS) payload safety requirements are identified to the ISS payload development organizations.
NSTS 1700.7B, SAFETY POLICY AND REQUIREMENTS FOR PAYLOADS USING THE SPACE TRANSPORTATION SYSTEM
NSTS 1700.7B, SAFETY POLICY AND REQUIREMENTS FOR PAYLOADS USING THE SPACE TRANSPORTATION SYSTEM. This document establishes the safety policy and requirements applicable to Space Transportation System and their ground support equipment (GSE).
Ident. Num:
NSTS 1700.7
Rev. Num:
B
NSTS 1700.7B, SAFETY POLICY AND REQUIREMENTS FOR PAYLOADS USING THE SPACE TRANSPORTATION SYSTEM. This document establishes the safety policy and requirements applicable to Space Transportation System and their ground support equipment (GSE).
NSTS 21000-IDD-MDK, MIDDECK INTERFACE DEFINITION DOCUMENT
NSTS 21000-IDD-MDK, MIDDECK INTERFACE DEFINITION DOCUMENT. This document defines and controls the design of interfaces between the Shuttle Orbiter and payloads that use Orbiter middeck payload accommodations.
Ident. Num:
NSTS 21000-IDD-MDK
Rev. Num:
B
NSTS 21000-IDD-MDK, MIDDECK INTERFACE DEFINITION DOCUMENT. This document defines and controls the design of interfaces between the Shuttle Orbiter and payloads that use Orbiter middeck payload accommodations.
NSTS 21492, SPACE SHUTTLE PROGRAM PAYLOAD BAY PAYLOAD USER'S GUIDE (BASIC)
NSTS/ISS 13830, PAYLOAD SAFETY REVIEW AND DATA SUBMITTAL REQUIREMENTS. This document contains information on the Space Shuttle system required by payload customers during the design definition, integration and flight phases for payload bay payloads. Payloads or experiments that will be using the middeck accommodations should refer to the Space Shuttle Program (SSP) Middeck Payload User’s Guide, NSTS TBD. The purpose of this document is to provide potential customers with information on Space Shuttle capability to deliver payloads into orbit and return them to Earth; on services provided to payload customers; and on the means by which payload customers can avail themselves of these services. Standard interface provisions between the Orbiter and payloads are also defined. With this information, payload planning and design studies can be undertaken incorporating known Shuttle capabilities and interface provisions. Additionally, information is provided on the process employed by the SSP to integrate individual payloads into the Shuttle, and the process of manifesting multiple payloads and providing for their integration into a Shuttle mission or flight. Additional information with hyperlinks to program documentation can be found at the Space Shuttle Payload Information System (SSPIS) web site.
Ident. Num:
NSTS 21492
Rev. Num:
-
NSTS/ISS 13830, PAYLOAD SAFETY REVIEW AND DATA SUBMITTAL REQUIREMENTS. This document contains information on the Space Shuttle system required by payload customers during the design definition, integration and flight phases for payload bay payloads. Payloads or experiments that will be using the middeck accommodations should refer to the Space Shuttle Program (SSP) Middeck Payload User’s Guide, NSTS TBD. The purpose of this document is to provide potential customers with information on Space Shuttle capability to deliver payloads into orbit and return them to Earth; on services provided to payload customers; and on the means by which payload customers can avail themselves of these services. Standard interface provisions between the Orbiter and payloads are also defined. With this information, payload planning and design studies can be undertaken incorporating known Shuttle capabilities and interface provisions. Additionally, information is provided on the process employed by the SSP to integrate individual payloads into the Shuttle, and the process of manifesting multiple payloads and providing for their integration into a Shuttle mission or flight. Additional information with hyperlinks to program documentation can be found at the Space Shuttle Payload Information System (SSPIS) web site.
NSTS 22648, FLAMMABILITY CONFIGURATION ANALYSIS FOR SPACECRAFT APPLICATIONS
NSTS 22648, FLAMMABILITY CONFIGURATION ANALYSIS FOR SPACECRAFT APPLICATIONS. The guidelines described herein are intended for assessment of flammability problems associated with air and oxygen-enriched environments in manned spacecraft.
Ident. Num:
NSTS 13830
Rev. Num:
-
NSTS 22648, FLAMMABILITY CONFIGURATION ANALYSIS FOR SPACECRAFT APPLICATIONS. The guidelines described herein are intended for assessment of flammability problems associated with air and oxygen-enriched environments in manned spacecraft.
NSTS/ISS 13830C, PAYLOAD SAFETY REVIEW AND DATA SUBMITTAL REQUIREMENTS
NSTS/ISS 13830C, PAYLOAD SAFETY REVIEW AND DATA SUBMITTAL REQUIREMENTS. The purpose of this document is to define the payload safety review process in order to assist the Shuttle/ISS POs in documenting compliance with the payload requirements documents specified in Section 1.
Ident. Num:
NSTS 13830
Rev. Num:
C
NSTS/ISS 13830C, PAYLOAD SAFETY REVIEW AND DATA SUBMITTAL REQUIREMENTS. The purpose of this document is to define the payload safety review process in order to assist the Shuttle/ISS POs in documenting compliance with the payload requirements documents specified in Section 1.
NSTS/ISS 18798B, INTERPRETATIONS OF NSTS/ISS PAYLOAD SAFETY REQUIREMENTS
NSTS/ISS 18798B, INTERPRETATIONS OF NSTS/ISS PAYLOAD SAFETY REQUIREMENTS. (Previously Titled NSTS 18798A). In implementing the payload safety review process, the Payload Safety Review Panel (PSRP) has been required to make interpretations of particular safety requirements. NSTS 18798 was issued to compile these letters into one document. The recent release of the International Space Station (ISS) Addendum to NSTS 1700.7B and other documentation changes dictate that this document be reissued and released as a joint SSP/ISS document. These letters will be utilized by the PSRP in assessing all payloads for design compliance. This release also deletes those letters made obsolete by changes in other documentation and reflects the applicability of each letter to the SSP and ISSP as necessary. Major reductions in the number of interpretation letters were made possible by the inclusion of their contents in other program documentation (see JSC 16979, “Failure Modes and Fault Tolerance for Orbiter,” and NASA-STD-5003, “Fracture Control Requirements for Payloads Using the Space Transportation System,” which replaces NHB 8071.1). This document is under joint control of both the SSP and ISSP and will be revised as necessary to reflect current interpretations of payload safety requirements. Future letters will contain an introductory paragraph clearly defining the program applicability. NSTS/ISS 18798 supersedes NSTS 18798 Revision A and has been organized to facilitate locating information by subject matter as shown in the topical index.
Ident. Num:
NSTS/ISS 18798
Rev. Num:
B
NSTS/ISS 18798B, INTERPRETATIONS OF NSTS/ISS PAYLOAD SAFETY REQUIREMENTS. (Previously Titled NSTS 18798A). In implementing the payload safety review process, the Payload Safety Review Panel (PSRP) has been required to make interpretations of particular safety requirements. NSTS 18798 was issued to compile these letters into one document. The recent release of the International Space Station (ISS) Addendum to NSTS 1700.7B and other documentation changes dictate that this document be reissued and released as a joint SSP/ISS document. These letters will be utilized by the PSRP in assessing all payloads for design compliance. This release also deletes those letters made obsolete by changes in other documentation and reflects the applicability of each letter to the SSP and ISSP as necessary. Major reductions in the number of interpretation letters were made possible by the inclusion of their contents in other program documentation (see JSC 16979, “Failure Modes and Fault Tolerance for Orbiter,” and NASA-STD-5003, “Fracture Control Requirements for Payloads Using the Space Transportation System,” which replaces NHB 8071.1). This document is under joint control of both the SSP and ISSP and will be revised as necessary to reflect current interpretations of payload safety requirements. Future letters will contain an introductory paragraph clearly defining the program applicability. NSTS/ISS 18798 supersedes NSTS 18798 Revision A and has been organized to facilitate locating information by subject matter as shown in the topical index.
