BS ISO 17770:2017

Foreword
Introduction
1 Scope
2 Normative references
3 Terms and definitions
4 Abbreviated terms
5 CubeSat requirements
6 Interface to the launch vehicle: The CubeSat Deployer
7 CubeSat and Deployer assurance/quality verification
Bibliography

Describes CubeSats, CubeSat Deployer and related verification of assurance/quality terms and metrics.

This document addresses CubeSats, CubeSat Deployer and related verification of assurance/quality terms and metrics.

This document defines a unique class of picosatellite, the CubeSat. CubeSats are ideal as space development projects for universities around the world. In addition to their significant role in educating space scientists and engineers, CubeSats provide a low-cost platform for testing and space qualification of the next generation of small payloads in space. A key component of the project is the development of a standard CubeSat Deployer.

This Deployer is capable of releasing a number of CubeSats as secondary payloads on a wide range of launchers. The standard Deployer requires all CubeSats to conform to common physical requirements, and share a standard Deployer interface. CubeSat development time and cost can be significantly reduced by the development of standards that are shared by a large number of spacecraft.

Normative control of the CubeSat design, qualification and acceptance testing is generally applied from other small satellite specific standards with the exception of CubeSat/Deployer launch environment test.