A NASA mission that will travel close to the sun requires a unique heatshield to protect the spacecraft and the instruments from the peak flux of 400 W/cm(sup 2) found at the mission's perihelion of 4 solar radii (~ 0.02 AU).
The Solar Probe Heatshield Development
Tri-Service Symposium on Advancements in Heatshield Technology
2000-05-10
Aufsatz (Konferenz)
Keine Angabe
Englisch
Jupiter Probe Heatshield design
AIAA | 1977
|Jupiter probe heatshield configuration optimization
AIAA | 1978
|