FAQ
FR
app.
— Mission Analysis
▸ Nodes
▸ Couplings
▸ Heaters
▸ Scenarios
▾ Transient run
hot case
eclipse
T [°C] — transient, 5 orbits
1U → 16U
200+
11
100%
🔒
01
Spacecraft
3U · double panel · 2 nodes
—
02
Mission Analysis
SSO 550 km · LTAN 10:30
—
03
Thermal Control
hot case
Transient · multi-node · 5 orbits
—
04
Quick Estimation
T_sink · +Z face
−12.4 °C
sol. 812 · alb. 96 · IR 118 W/m²
GL · 4 x M2 + 2 x M3
0.94 W/K
bolted contact · series GL₁·GL₂·GL₃
Radiator required
2.1 dm²
ε 0.80 · margin +6 °C
3-node electronics box
PCB 47 °C
8πλt spreading · walls
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1
Spacecraft
2
Mission Analysis
3
Thermal Control
4
Report
⚡
Quick Estimation
FAQ
