EURECA Thermal Control Subsystem Concept

840963

07/01/1984

Event
Intersociety Conference on Environmental Systems
Authors Abstract
Content
EURECA (EUropean REtrievable CArrier) is the first European reusable platform with the purpose of carrying into space multidisciplinary payloads. The first mission is dedicated to micro gravity with experiments on material processing and life science.
EURECA will be placed in orbit by the Space Shuttle and retrieved after a period of 6 to 9 months. Since its operating altitude is 500 km (circular orbit) the residual acceleration is expected to be lower than 10−5g. The first EURECA mission is scheduled for 1987 and 5 missions are planned in 10 years.
AERITALIA is responsible of the platform Thermal Control Subsystem the design of which has to fulfill a wide range of temperature requirements for both the payloads and the subsystem equipments. The boundary conditions to be considered in the thermal design are dictated by the different mission phases (ascent, in cargo-bay conditions, deployment, transfer orbit, in orbit operational and dormant phases, retrieval and descent phases).
The Thermal Control is achieved by active (heat rejection through fluid radiator panels) and passive (multilayer thermal blankets, heaters and paints) means. The applied technology has mainly been developed during the SPACELAB program and most of the used components are already qualified hardware.
Meta TagsDetails
DOI
https://doi.org/10.4271/840963
Pages
8
Citation
Costamagna, L., and Brambati, G., "EURECA Thermal Control Subsystem Concept," SAE Technical Paper 840963, 1984, https://doi.org/10.4271/840963.
Additional Details
Publisher
Published
Jul 1, 1984
Product Code
840963
Content Type
Technical Paper
Language
English