ISO 17401:2004
Space systems — Spacecraft interface requirements document for launch vehicle services
ISO 17401:2004 provides spacecraft (SC) organizations with the general format for presenting the interface requirement document (IRD) for launch vehicle services. The IRD provides a list of the major technical requirements spacecraft agencies provide to launch vehicle (LV) agencies when submitting an application for launch services.
ISO 17401:2004 is applicable to all existing commercial LV and related launch facilities so as to permit SC contractors to prepare a single interface requirement document for a given SC mission, independently of the LV contractor to be selected.
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TitlePage - Space systems— Spacecraft interface requirements document for launch vehicle services
TableofContent - Contents Page
Foreword - Foreword
Introduction - Introduction
Scope - 1 Scope
Clause1 - 2 Terms, definitions and abbreviated terms
Clause1 - 3 Spacecraft mission description
Subclause2 - 3.1 Mission description
Subclause2 - 3.2 SC description
Clause1 - 4 Mechanical interfaces
Subclause2 - 4.1 Mechanical configuration
Subclause2 - 4.2 SC fundamental frequencies
Subclause2 - 4.3 Usable volume
Subclause2 - 4.4 Spacecraft (or SC adapter) mechanical interface
Subclause2 - 4.5 Connectors and microswitches (SC side of the interface)
Subclause2 - 4.6 Purges and fluid connection interface
Subclause2 - 4.7 Encapsulated spacecraft access
Clause1 - 5 Electrical interfaces
Subclause2 - 5.1 Umbilical wiring diagram
Subclause2 - 5.2 Umbilical connectors
Subclause2 - 5.3 Umbilical wiring links (for each connector pin)
Subclause2 - 5.4 Electrical commands dedicated to spacecraft
Subclause3 - 5.4.1 Pyrotechnic commands
Subclause3 - 5.4.2 Dry loop commands
Subclause3 - 5.4.3 Electrical commands
Subclause2 - 5.5 Separation status transmission
Subclause2 - 5.6 SC in-flight telemetry
Subclause2 - 5.7 Power supply required from LV
Subclause2 - 5.8 Earth potential continuity
Clause1 - 6 Radio-frequency and electromagnetic interface
Subclause2 - 6.1 Characteristics of radio-electrical systems
Subclause2 - 6.2 RF telemetry and command link
Subclause3 - 6.2.1 SC RF-link definition for ground operations
Subclause3 - 6.2.2 SC antenna coordinates
Subclause3 - 6.2.3 RF-link implementation
Subclause3 - 6.2.4 RF-link budget
Subclause3 - 6.2.5 Base band signal characteristics
Clause1 - 7 Spacecraft mission characteristics
Subclause2 - 7.1 SC input data for mission analyses
Subclause3 - 7.1.1 Mass and inertia characteristics
Subclause3 - 7.1.2 Sloshing masses (pendulum-type)
Subclause3 - 7.1.3 SC mission constraints (when applicable)
Subclause2 - 7.2 SC orbit parameters (with tolerances)
Subclause2 - 7.3 Launch window
Subclause3 - 7.3.1 Launch window constraints (when applicable)
Subclause3 - 7.3.2 Preferred window
Subclause2 - 7.4 SC pointing and separation
Clause1 - 8 Environment requirements
Subclause2 - 8.1 General
Subclause2 - 8.2 Mechanical environment
Subclause2 - 8.3 Thermal environment
Subclause2 - 8.4 Static pressure
Subclause2 - 8.5 Contamination and cleanliness control
Subclause2 - 8.6 Radio frequency and electromagnetic environment
Subclause2 - 8.7 Environment monitoring
Clause1 - 9 SC Development and test programme
Subclause2 - 9.1 Mechanical environment qualification tests
Subclause2 - 9.2 LV/SC compatibility tests
Clause1 - 10 Launch range operations: facilities and support requirements
Subclause2 - 10.1 General logistics requirements
Subclause3 - 10.1.1 General
Subclause3 - 10.1.2 SC container and ground support equipment physical envelopes
Subclause3 - 10.1.3 Material handling equipment
Subclause3 - 10.1.4 Electrical power for SC and ground station
Subclause3 - 10.1.5 Umbilical lines and ground lines
Subclause3 - 10.1.6 Gas and fluid lines
Subclause3 - 10.1.7 Clean room
Subclause3 - 10.1.8 Environmental controls for SC and ground station
Subclause3 - 10.1.9 Clothing (safety and cleanroom)
Subclause3 - 10.1.10 Area
Subclause3 - 10.1.11 Storage (non hazardous items)
Subclause3 - 10.1.12 SC pre-launch activities calendar
Subclause3 - 10.1.13 Special technical support equipment
Subclause3 - 10.1.14 Other
Subclause2 - 10.2 Specific requirements for solid propellant motor facilities (Y/N, to specify)
Subclause3 - 10.2.1 Solid propellant motor storage
Subclause3 - 10.2.2 Pyrotechnics storage
Subclause2 - 10.3 Specific requirements for X-ray facilities
Subclause2 - 10.4 Specific requirements for hazardous operations facilities
Subclause3 - 10.4.1 Gases
Subclause3 - 10.4.2 Liquid propellant
Subclause3 - 10.4.3 SC purge requirements
Subclause3 - 10.4.4 SC fluid requirements
Subclause2 - 10.5 Payload handling and transport requirements
Subclause2 - 10.6 Communication requirements
Subclause2 - 10.7 General range services
Clause1 - 11 Other requirements
Bibliography - Bibliography
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TitlePage - Space systems— Spacecraft interface requirements document for launch vehicle services
TableofContent - Contents Page
Foreword - Foreword
Introduction - Introduction
Scope - 1 Scope
Clause1 - 2 Terms, definitions and abbreviated terms
Clause1 - 3 Spacecraft mission description
Subclause2 - 3.1 Mission description
Subclause2 - 3.2 SC description
Clause1 - 4 Mechanical interfaces
Subclause2 - 4.1 Mechanical configuration
Subclause2 - 4.2 SC fundamental frequencies
Subclause2 - 4.3 Usable volume
Subclause2 - 4.4 Spacecraft (or SC adapter) mechanical interface
Subclause2 - 4.5 Connectors and microswitches (SC side of the interface)
Subclause2 - 4.6 Purges and fluid connection interface
Subclause2 - 4.7 Encapsulated spacecraft access
Clause1 - 5 Electrical interfaces
Subclause2 - 5.1 Umbilical wiring diagram
Subclause2 - 5.2 Umbilical connectors
Subclause2 - 5.3 Umbilical wiring links (for each connector pin)
Subclause2 - 5.4 Electrical commands dedicated to spacecraft
Subclause3 - 5.4.1 Pyrotechnic commands
Subclause3 - 5.4.2 Dry loop commands
Subclause3 - 5.4.3 Electrical commands
Subclause2 - 5.5 Separation status transmission
Subclause2 - 5.6 SC in-flight telemetry
Subclause2 - 5.7 Power supply required from LV
Subclause2 - 5.8 Earth potential continuity
Clause1 - 6 Radio-frequency and electromagnetic interface
Subclause2 - 6.1 Characteristics of radio-electrical systems
Subclause2 - 6.2 RF telemetry and command link
Subclause3 - 6.2.1 SC RF-link definition for ground operations
Subclause3 - 6.2.2 SC antenna coordinates
Subclause3 - 6.2.3 RF-link implementation
Subclause3 - 6.2.4 RF-link budget
Subclause3 - 6.2.5 Base band signal characteristics
Clause1 - 7 Spacecraft mission characteristics
Subclause2 - 7.1 SC input data for mission analyses
Subclause3 - 7.1.1 Mass and inertia characteristics
Subclause3 - 7.1.2 Sloshing masses (pendulum-type)
Subclause3 - 7.1.3 SC mission constraints (when applicable)
Subclause2 - 7.2 SC orbit parameters (with tolerances)
Subclause2 - 7.3 Launch window
Subclause3 - 7.3.1 Launch window constraints (when applicable)
Subclause3 - 7.3.2 Preferred window
Subclause2 - 7.4 SC pointing and separation
Clause1 - 8 Environment requirements
Subclause2 - 8.1 General
Subclause2 - 8.2 Mechanical environment
Subclause2 - 8.3 Thermal environment
Subclause2 - 8.4 Static pressure
Subclause2 - 8.5 Contamination and cleanliness control
Subclause2 - 8.6 Radio frequency and electromagnetic environment
Subclause2 - 8.7 Environment monitoring
Clause1 - 9 SC Development and test programme
Subclause2 - 9.1 Mechanical environment qualification tests
Subclause2 - 9.2 LV/SC compatibility tests
Clause1 - 10 Launch range operations: facilities and support requirements
Subclause2 - 10.1 General logistics requirements
Subclause3 - 10.1.1 General
Subclause3 - 10.1.2 SC container and ground support equipment physical envelopes
Subclause3 - 10.1.3 Material handling equipment
Subclause3 - 10.1.4 Electrical power for SC and ground station
Subclause3 - 10.1.5 Umbilical lines and ground lines
Subclause3 - 10.1.6 Gas and fluid lines
Subclause3 - 10.1.7 Clean room
Subclause3 - 10.1.8 Environmental controls for SC and ground station
Subclause3 - 10.1.9 Clothing (safety and cleanroom)
Subclause3 - 10.1.10 Area
Subclause3 - 10.1.11 Storage (non hazardous items)
Subclause3 - 10.1.12 SC pre-launch activities calendar
Subclause3 - 10.1.13 Special technical support equipment
Subclause3 - 10.1.14 Other
Subclause2 - 10.2 Specific requirements for solid propellant motor facilities (Y/N, to specify)
Subclause3 - 10.2.1 Solid propellant motor storage
Subclause3 - 10.2.2 Pyrotechnics storage
Subclause2 - 10.3 Specific requirements for X-ray facilities
Subclause2 - 10.4 Specific requirements for hazardous operations facilities
Subclause3 - 10.4.1 Gases
Subclause3 - 10.4.2 Liquid propellant
Subclause3 - 10.4.3 SC purge requirements
Subclause3 - 10.4.4 SC fluid requirements
Subclause2 - 10.5 Payload handling and transport requirements
Subclause2 - 10.6 Communication requirements
Subclause2 - 10.7 General range services
Clause1 - 11 Other requirements
Bibliography - Bibliography