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Thermal Protection System
High-temperature and Cryogenic Thermal Protection Systems to protect satellite launch vehicles.
※ Accumulation of unrivaled technology in thermal protection systems, the only specialized contractor in the launch vehicle insulation field.
※ Accumulation of unrivaled technology in thermal protection systems, the only specialized contractor in the launch vehicle insulation field.
Installation of Insulation for Satellite Launch Vehicle (Nuri)
| No | Equipment Name | Satellite | Remarks |
|---|---|---|---|
| 1st - 3rd Launch | Oct '21 ~ May '23 | 1.3-ton ~ 1.5-ton Satellite Simulator, Next-Generation Small Satellite (SNIPE) | Completed |
| 4th Launch | Nov '25 ~ Dec '25 | Next-Generation Medium Satellite No. 3, Innospace Private Launch Vehicle | Completed |
| 5th - 6th Launch | Oct '21 ~ May '23 | Micro-satellites No. 2-11 | Scheduled |
Insulation application in progress during the 3rd launch
KUH Engine: Supplying Engine Cover Insulation for KUH Mass Production ('14 - Present)
KSLV-II Thermal Protection System
High-temperature Insulation (Aft Fuselage)
Usage
Protects launch vehicle structures from plume heating
Performance
Protection in -250°C - 290°C (-420°F - 550°F) environments
Description
Manufactured using the “Multi Layer Insulator” method to prevent conduction and radiant heat transfer.
High-temperature Insulation (Aft Fuselage)
Usage
Protects launch vehicle structures from plume heating
Performance
Protection in -250°C - 290°C (-420°F - 550°F) environments
Description
Manufactured using the “Multi Layer Insulator” method to prevent conduction and radiant heat transfer.
High-temperature Insulation (Aft Fuselage)
Usage
Protects launch vehicle structures from plume heating
Performance
Protection in -250°C - 290°C (-420°F - 550°F) environments
Description
Manufactured using the “Multi Layer Insulator” method to prevent conduction and radiant heat transfer.
