2nd Thermophysics Specialist Conference 1967
DOI: 10.2514/6.1967-329
|View full text |Cite
|
Sign up to set email alerts
|

Role of flight experiments in the study of thermal-control coatings for spacecraft

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...

Citation Types

0
1
0

Year Published

1967
1967
1969
1969

Publication Types

Select...
2
1
1

Relationship

0
4

Authors

Journals

citations
Cited by 4 publications
(1 citation statement)
references
References 11 publications
0
1
0
Order By: Relevance
“…6 It has been tested on flight vehicles, namely, Pesagus II and III, 6 on OSO IF (with slight modifications in the coating), and is scheduled for use on the radiators for the service module of the Apollo vehicle. 8 The results of these tests and its relative ease of application, good mechanical properties, and adequate adhesion to most spacecraft surfaces have indicated its adequacy for space use. However, it is essentially a ceramic and can be chipped by mishandling.…”
mentioning
confidence: 95%
“…6 It has been tested on flight vehicles, namely, Pesagus II and III, 6 on OSO IF (with slight modifications in the coating), and is scheduled for use on the radiators for the service module of the Apollo vehicle. 8 The results of these tests and its relative ease of application, good mechanical properties, and adequate adhesion to most spacecraft surfaces have indicated its adequacy for space use. However, it is essentially a ceramic and can be chipped by mishandling.…”
mentioning
confidence: 95%