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mission
Definition
a possible instantiation of the mission statement in a mission conceptNotes
- NOTE 1 Each mission is described in an MDD
- NOTE 2 The implementation in time is called mission scenario.
Relations
- ECSS-S-ST-00-01C — accident
- ECSS-E-ST-70-11C — commandability
- ECSS-M-ST-10-01C — consumer
- ECSS-E-ST-10-11C — crew
- ECSS-S-ST-00-01C — critical
- ECSS-Q-ST-70-39C — critical structure
- ECSS-E-ST-70-11C — deactivation
- ECSS-E-ST-32C Rev. 1 — detrimental deformation
- ECSS-E-ST-35C Rev. 1 — dimensioning
- ECSS-S-ST-00-01C — embedded space segment element
- ECSS-E-ST-70-32C — EMCS
- ECSS-E-ST-70-31C — EMCS
- ECSS-E-ST-10-12C — EPIC
- ECSS-E-ST-10-12C — ESABASE
- ECSS-E-ST-70-32C — event
- ECSS-E-ST-70-31C — event
- ECSS-E-ST-33-11C Rev.1 — fail operational
- ECSS-E-ST-70C — ground segment
- ECSS-Q-ST-30-09C — ground segment
- ECSS-E-ST-70C — ground system
- ECSS-U-ST-20C — inbound leg
- ECSS-S-ST-00-01C — launcher stage
- ECSS-E-ST-31C — limit aero-thermal heat flux
- ECSS-Q-ST-30C Rev.1 — limited-life product
- ECSS-E-ST-32-01C Rev. 1 — loading event
- ECSS-E-ST-70-11C — loss of mission
- ECSS-E-ST-70C — MAR
- ECSS-E-ST-32C Rev. 1 — maximum expected operating pressure (MEOP)
- ECSS-S-ST-00-01C — MCR
- ECSS-E-ST-10C Rev.1 — MCR
- ECSS-E-ST-70C — MCR
- ECSS-M-ST-10C Rev. 1 — MCR
- ECSS-E-ST-70-01C — MCS
- ECSS-S-ST-00-01C — MDD
- ECSS-E-ST-70C — MDD
- ECSS-E-ST-10C Rev.1 — MDD
- ECSS-E-ST-10-06C — MDD
- ECSS-S-ST-00-01C — MDR
- ECSS-M-ST-10C Rev. 1 — MDR
- ECSS-E-ST-10C Rev.1 — MDR
- ECSS-E-ST-50C — MEC
- ECSS-Q-ST-70-39C — mission critical
- ECSS-E-ST-70C — mission exploitation
- ECSS-E-ST-70C — mission operations data
- ECSS-E-ST-50-03C — mission phase
- ECSS-E-ST-50-04C — mission phase
- ECSS-E-ST-40-07C — mission time
- ECSS-E-ST-70-11C — mission-critical function
- ECSS-M-ST-40C Rev. 1 — MOB
- ECSS-E-ST-70C — MOCD
- ECSS-E-ST-70C — MOP
- ECSS-E-ST-10C Rev.1 — MOP
- ECSS-E-ST-60-30C — MRD
- ECSS-M-ST-10-01C — MRD
- ECSS-E-ST-70C — MRT
- ECSS-E-ST-10C Rev.1 — MS
- ECSS-E-ST-31C — natural environment
- ECSS-E-ST-31C — nominal aero-thermal heat fluxes
- ECSS-E-ST-70-11C — operability
- ECSS-E-ST-70C — operational validation
- ECSS-E-ST-70-11C — operations
- ECSS-E-ST-10-11C — operations nomenclature
- ECSS-U-ST-20C — outbound leg
- ECSS-E-ST-70-11C — permanent degradation of space segment function
- ECSS-E-ST-70-11C — permanent mission degradation
- ECSS-U-ST-20C — planetary protection category
- ECSS-E-ST-10-11C — procedure
- ECSS-E-ST-35C Rev. 1 — propellant gauging
- ECSS-E-ST-31C — qualification test (system level)
- ECSS-Q-ST-70-29C — rack
- ECSS-E-ST-10-12C — radiation design margin (RDM)
- ECSS-E-ST-10-12C — radiation design margin (RDM)
- ECSS-S-ST-00-01C — segment
- ECSS-E-ST-20-08C Rev. 1 — slicing
- ECSS-E-ST-31-04C — SMA
- ECSS-S-ST-00-01C — space mission
- ECSS-S-ST-00-01C — space segment
- ECSS-S-ST-00-01C — stand-alone space segment element
- ECSS-E-ST-70-32C — statement
- ECSS-E-ST-70-11C — temporary mission degradation
- ECSS-Q-ST-60-15C — total ionizing dose level (TIDL)
- ECSS-Q-ST-60-15C — total non-ionizing dose level (TNIDL)
- ECSS-E-ST-70-11C — vital function
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