Infoteenus
49 LENNUNDUS JA KOSMOSETEHNIKA
Uued standardid
ISO 23312:2026
Space systems — Detailed space debris mitigation requirements for spacecraft
Käsitlusala: This document defines detailed space debris mitigation requirements and recommendations for the design and operation of unmanned spacecraft in Earth orbit.
This document defines detailed requirements that are applicable to:
avoiding the intentional release of space debris into Earth orbit during normal operations;
avoiding break-ups in Earth orbit;
disposal of a spacecraft after the end of mission;
estimating the mass of the remaining usable propellant;
developing and maintaining the space debris mitigation plan.
NOTE This document does not cover nuclear power sources on spacecraft.
This document defines detailed requirements that are applicable to:
avoiding the intentional release of space debris into Earth orbit during normal operations;
avoiding break-ups in Earth orbit;
disposal of a spacecraft after the end of mission;
estimating the mass of the remaining usable propellant;
developing and maintaining the space debris mitigation plan.
NOTE This document does not cover nuclear power sources on spacecraft.
Alusdokumendid:
Asendab: ISO 23312:2022
Asendatud standardid
ISO 23312:2022
Space systems — Detailed space debris mitigation requirements for spacecraft
Käsitlusala: This document defines detailed space debris mitigation requirements and recommendations for the design and operation of unmanned spacecraft in Earth orbit.
This document defines detailed requirements that are applicable to:
a) avoiding the intentional release of space debris into Earth orbit during normal operations;
b) avoiding break-ups in Earth orbit;
c) disposal of a spacecraft after the end of mission;
d) estimating the mass of the remaining usable propellant;
e) developing and maintaining the space debris mitigation plan.
NOTE This document does not cover nuclear power sources on spacecraft.
This document defines detailed requirements that are applicable to:
a) avoiding the intentional release of space debris into Earth orbit during normal operations;
b) avoiding break-ups in Earth orbit;
c) disposal of a spacecraft after the end of mission;
d) estimating the mass of the remaining usable propellant;
e) developing and maintaining the space debris mitigation plan.
NOTE This document does not cover nuclear power sources on spacecraft.
Alusdokumendid:
Asendatud: ISO 23312:2026
Kavandid
prEN 3682-001
Aerospace series - Connectors, plug and receptacle, electrical, rectangular, interchangeable insert type, rack to panel, operating temperature 150 °C continuous - Part 001: Technical specification
Käsitlusala: This document specifies the general characteristics, the conditions for qualification, acceptance and quality assurance, as well as the test programs and groups for connectors intended for use in a temperature range from - 65 °C to 150 °C continuous.
Alusdokumendid: prEN 3682-001
prEN 3682-002
Aerospace series - Connectors, plug and receptacle, electrical, rectangular, interchangeable insert type, rack to panel, operating temperature 150 °C continuous - Part 002: Specification of performance and contact arrangements
Käsitlusala: This document specifies the common conditions for plug and receptacle, rack to panel with interchangeable insulators and continuous temperature rating 150 °C.
Alusdokumendid: prEN 3682-002