AI Chat Paper
Note: Please note that the following content is generated by AMiner AI. SciOpen does not take any responsibility related to this content.
{{lang === 'zh_CN' ? '文章概述' : 'Summary'}}
{{lang === 'en_US' ? '中' : 'Eng'}}
Chat more with AI
PDF (448.5 KB)
Collect
Submit Manuscript AI Chat Paper
Show Outline
Outline
Show full outline
Hide outline
Outline
Show full outline
Hide outline

Propulsion Challenges for Small Spacecraft: 2005

Vadim Zakirov( )Luming LI
Tsinghua Space Center, School of Aerospace, Tsinghua University, Beijing 100084, China
Show Author Information

Abstract

Small (<100 kg) spacecrafts are being developed in many countries but their propulsion systems still have many challenges. Although there is demand for small spacecraft propulsion, the number of missions at present is small due to several commercial and technical reasons. Poor performance of existing small spacecraft propulsion systems is one of the main reasons for the small number of missions. Several reasons are given for the poor performance of existing small spacecraft propulsion. Suggested improvements focus on small spacecraft and propulsion hardware mass optimization rather than on specific impulse enhancement. Propellantless propulsion systems are also recommended for small spacecraft interplanetary missions.

References

【1】
【1】
 
 
Tsinghua Science and Technology
Pages 507-514

{{item.num}}

Comments on this article

Go to comment

< Back to all reports

Review Status: {{reviewData.commendedNum}} Commended , {{reviewData.revisionRequiredNum}} Revision Required , {{reviewData.notCommendedNum}} Not Commended Under Peer Review

Review Comment

Close
Close
Cite this article:
Zakirov V, LI L. Propulsion Challenges for Small Spacecraft: 2005. Tsinghua Science and Technology, 2006, 11(5): 507-514. https://doi.org/10.1016/S1007-0214(06)70227-9

0

Views

0

Downloads

0

Crossref

N/A

Web of Science

0

Scopus

0

CSCD

Received: 16 May 2005
Revised: 25 November 2005
Published: 01 October 2006
© Tsinghua University Press 2006