1998-07-13

Thermal Design of the International Space Station Photovoltaic Radiators 981728

The Photovoltaic Radiator (PVR) is designed to reject waste heat of the Early External Active Thermal Control System (EEATCS) and the Photovoltaic Thermal Control System (PV TCS) of the International Space Station (ISS). Two EEATCS PVR units and one PV TCS PVR unit will be on the Assured Early Research (AER) phase of the ISS and all four PV TCS PVR units will be on the assembly complete configuration of the ISS. Thermal environments of the AER mission and assembly complete configuration present challenging thermal designs to maintain the EEATCS and PV TCS PVR units functioning within the temperature operating limits of the structural components and the ammonia fluid.

SAE MOBILUS

Subscribers can view annotate, and download all of SAE's content. Learn More »

Access SAE MOBILUS »

Members save up to 16% off list price.
Login to see discount.
Special Offer: Download multiple Technical Papers each year? TechSelect is a cost-effective subscription option to select and download 12-100 full-text Technical Papers per year. Find more information here.
We also recommend:
TECHNICAL PAPER

Space Station External Thermal Control System Design and Operational Overview

921106

View Details

TECHNICAL PAPER

A Selected Operational History of the Internal Thermal Control System (ITCS) for International Space Station (ISS)

2004-01-2470

View Details

TECHNICAL PAPER

Development of the Internal Thermal Control System (ITCS) for International Space Station (ISS)

2001-01-2332

View Details

X