Compatibility measurements were made for aluminum 2219-T87 alloy and titanium 6Al-4V alloy in the presence of liquid fluorine and flox. Results of post test characterization after exposure durations of 61 and 70 weeks are presented. Results of the total test program are analyzed.
Compatibility testing of spacecraft materials and space-storable liquid propellants
1974-05-01
Report
No indication
English
Earth-storable propellants for spacecraft.
NTRS | 1965
|Earth-storable propellants for spacecraft
Engineering Index Backfile | 1965
|