ISO 15863:2003
Current
The latest, up-to-date edition.
Space systems Spacecraft-to-launch-vehicle interface control document
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English, French
30-10-2003
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The purpose of ISO 15863:2003 is to provide spacecraft (SC) and launch vehicle (LV) organizations with the general format for presenting the interface control document (ICD) that verifies and controls the compatibility between SC and LV for a dedicated mission. ISO 15863:2003 addresses the definition of the mission, the compatibility of the SC with the LV environment, including all mechanical, electrical, radio frequency, and electromagnetic aspects related to SC to LV and SC to launch range interfaces, verification analyses and tests for the induced environment, and the necessary facilities and support for launch range operations.
| DevelopmentNote |
Supersedes ISO/DIS 15863 (10/2003)
|
| DocumentType |
Standard
|
| Pages |
28
|
| PublisherName |
International Organization for Standardization
|
| Status |
Current
|
| Standards | Relationship |
| BS ISO 15863:2003 | Identical |
| 10/30240189 DC : 0 | BS ISO 26869 - SPACE SYSTEMS - SMALL AUXILIARY SPACECRAFT TO LAUNCH VEHICLE INTERFACE CONTROL DOCUMENT |
| BS ISO 19933:2007 | Space systems. Format for spacecraft launch environment test report |
| BS ISO 17689:2015 | Space systems. Interface control documents between ground systems, ground support equipment and launch vehicle with payload |
| ISO 26869:2012 | Space systems — Small-auxiliary-spacecraft (SASC)-to- launch- vehicle interface control document |
| 10/30197704 DC : 0 | BS ISO 10784-2 - SPACE SYSTEMS - EARLY OPERATIONS - PART 2: INITIALIZATION PLAN |
| BS ISO 16458:2004 | Space systems. Unmanned spacecraft transportation. General requirements |
| BS ISO 10784-2:2011 | Space systems. Early operations Initialization plan |
| 03/305725 DC : DRAFT APR 2003 | ISO 15864 - SPACE SYSTEMS - UNMANNED SPACECRAFT DESIGN, PERFORMANCE AND QUALITY ASSESSMENT - GENERAL TEST METHODS FOR SYSTEM, SUBSYSTEM AND UNIT LEVELS |
| PD ISO/TR 19473:2015 | Space systems. Best practices for orbit elements at payload. LV separation |
| 02/706706 DC : DRAFT MAY 2002 | BS ISO 16458 - SPACE SYSTEMS - UNMANNED SPACECRAFT TRANSPORTATION - GENERAL REQUIREMENTS |
| 06/30140973 DC : DRAFT JUN 2006 | ISO 19933 - SPACE SYSTEMS - FORMAT FOR SPACECRAFT LAUNCH ENVIRONMENT TEST REPORT |
| ISO 19933:2007 | Space systems Format for spacecraft launch environment test report |
| ISO 10784-2:2011 | Space systems Early operations Part 2: Initialization plan |
| ISO 10784-3:2011 | Space systems Early operations Part 3: Commissioning report |
| 08/30176277 DC : DRAFT JAN 2008 | BS ISO 15862 - SPACE SYSTEMS - SPACECRAFT-TO-LAUNCH-VEHICLE FLIGHT ENVIRONMENTS TELEMETRY DATA PROCESSING |
| BS ISO 10784-3:2011 | Space systems. Early operations Commissioning report |
| 10/30197707 DC : 0 | BS ISO 10784-3 - SPACE SYSTEMS - EARLY OPERATIONS - PART 3: COMMISSIONING REPORT |
| BS ISO 10784-1:2011 | Space systems. Early operations Spacecraft initialization and commissioning |
| ISO 16458:2004 | Space systems — Unmanned spacecraft transportation — General requirements |
| ISO 17689:2015 | Space systems — Interface control documents between ground systems, ground support equipment and launch vehicle with payload |
| 14/30289416 DC : 0 | BS ISO 17689 - SPACE SYSTEMS - INTERFACE CONTROL DOCUMENTS BETWEEN GROUND SYSTEMS, GROUND SUPPORT EQUIPMENT AND LAUNCH VEHICLE WITH PAYLOAD |
| 02/709704 DC : DRAFT AUG 2002 | ISO/DIS 17401 - SPACE SYSTEMS - DOCUMENTS FOR SPACE CRAFT INTERFACE REQUIREMENTS FOR LAUNCH VEHICLE SERVICES |
| ISO 17401:2004 | Space systems — Spacecraft interface requirements document for launch vehicle services |
| BS ISO 26869:2012 | Space systems. Small-auxiliary-spacecraft (SASC) to-launch-vehicle interface control document |
| 10/30197700 DC : 0 | BS ISO 10784-1 - SPACE SYSTEMS - EARLY OPERATIONS - PART 1: SPACECRAFT INITIALIZATION AND COMMISSIONING |
| ISO/TR 19473:2015 | Space systems Best practices for orbit elements at payload LV separation |
| ISO 10784-1:2011 | Space systems Early operations Part 1: Spacecraft initialization and commissioning |
| ISO 14303:2002 | Space systems — Launch-vehicle-to-spacecraft interfaces |
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