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Deployment Systems

  • ISIS-Innovative Solutions In Space B.V.
  • California Polytechnic State University, San Luis Obispo

Research output: Chapter in Book/Report/Conference proceedingChapterpeer-review

1 Citation (Scopus)

Abstract

This chapter introduces various nanosatellite deployment systems. Nanosatellites are generally designed and developed based on the CubeSat standard and usually launched using a picosatellite orbital deployer (POD), a special container originally called ‘poly picosatellite orbital deployer (P-POD). The deployment system provides a standard interface between a nanosatellite and a launch vehicle. The deployment system tasks are: to enclose safer environment of the nanosatellite, to protect the main payload and the rocket from possible damages, to act as an interface between the nanosatellite and the launch vehicle, and to deploy the satellites to the target orbit. The chapter discusses existing deployers and their properties. The deployers are P-POD, T-POD, XPOD separation system, ISIPOD CubeSat deployers, OuadPack ISIS deployer, JEM-small satellite orbital deployer, SPL/DPL/TPL, Tokyo tech separation system, and AxelShooter.

Original languageEnglish
Title of host publicationNanosatellites
Subtitle of host publicationSpace and Ground Technologies, Operations and Economics
Publisherwiley
Pages375-397
Number of pages23
ISBN (Electronic)9781119042044
ISBN (Print)9781119042037
DOIs
Publication statusPublished - 1 Jan 2020

Bibliographical note

Publisher Copyright:
© 2020 John Wiley & Sons Ltd. All rights reserved.

Keywords

  • CubeSat standard
  • T-POD
  • XPOD separation system
  • launch vehicle
  • nanosatellite deployment systems
  • picosatellite orbital deployer

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