SAE Technical Paper Series 2004
DOI: 10.4271/2004-01-2507
|View full text |Cite
|
Sign up to set email alerts
|

Current Mechanically Pumped Two-Phase Thermal Control Loop Developments

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
2

Citation Types

0
2
0

Year Published

2005
2005
2023
2023

Publication Types

Select...
3
1
1

Relationship

0
5

Authors

Journals

citations
Cited by 7 publications
(2 citation statements)
references
References 13 publications
0
2
0
Order By: Relevance
“…However, employing the same system for small satellites and nanosatellites ranging from 10 kg to 100 kg increases the risk to a higher degree. Conventional mechanically pumped thermal control fluid loop systems are single-phase [Delil, 2004b], relying on the heat capacity of the working fluid.…”
Section: Mpfl In Conventional Satellite Missions -Reviewmentioning
confidence: 99%
See 1 more Smart Citation
“…However, employing the same system for small satellites and nanosatellites ranging from 10 kg to 100 kg increases the risk to a higher degree. Conventional mechanically pumped thermal control fluid loop systems are single-phase [Delil, 2004b], relying on the heat capacity of the working fluid.…”
Section: Mpfl In Conventional Satellite Missions -Reviewmentioning
confidence: 99%
“…MPFL with freon-11 was chosen for MPF's HRS due to its following attractive features. [Delil, 2004b]: 1) Ease of integration with the spacecraft, 2) No orientation constraints, 3) Control temperatures of remotely located components, 4) Modulate the system's temperature with changing environmental conditions and equipment power, 5) Versatile thermal control system for future missions (Smaller in size, cheaper, and lighter). Since then, MPFL has been used in various space exploration missions.…”
Section: Mpfl In Conventional Satellite Missions -Reviewmentioning
confidence: 99%