Results 241 to 250 of about 9,648,016 (296)
Some of the next articles are maybe not open access.

Thermal Balance Test of the EuTEF Payload

SAE Technical Paper Series, 2007
<div class="htmlview paragraph">This paper describes the Thermal Balance test that has been performed on EuTEF (European Technology Exposure Facility) platform, to be flown in October 2007 as an attached payload of Columbus module to the ISS.</div> <div class="htmlview paragraph">The thermal control system of EuTEF is based on a ...
Christian Vettore, Marco Molina
openaire   +1 more source

INTEGRAL Spectrometer Thermal Balance Test

SAE Technical Paper Series, 2000
<div class="htmlview paragraph">This paper describes the thermal balance test which has been performed on the spectrometer SPI Structural and Thermal Model (INTEGRAL project) from August 27<sup>th</sup> to September 17<sup>th</sup> 1999. Main SPI modes have been simulated in order to qualify the instrument thermal control.&
Fabienne Serène   +2 more
openaire   +1 more source

Thermal Balance Test of the PAMELA Telescope

SAE Technical Paper Series, 2004
<div class="htmlview paragraph">This paper describes the Thermal Balance test that has been performed on the PAMELA telescope Pressurized Container (PC) to verify the performance of the PC Thermal Control System (TCS). The PC will be attached outside the Russian satellite RESOURS DK to be flown in2004</div> <div class="htmlview paragraph"
Christian Vettore   +4 more
openaire   +1 more source

METOP PLM Thermal Balance and Thermal Vacuum Test

SAE Technical Paper Series, 2003
<div class="htmlview paragraph">This paper reports on the thermal testing of METOP (<b>MET</b>erological <b>OP</b>erational satellite) Payload Module Engineering Model, conducted in May/June 2001 at ESTEC’s Large Space Simulator (LSS).</div> <div class="htmlview paragraph">The paper describes the logic for the ...
Jürgen Schilke   +2 more
openaire   +1 more source

AGILE Satellite Thermal Balance and Thermal Vacuum Test

SAE Technical Paper Series, 2007
<div class="htmlview paragraph">This paper reports on the thermal testing of <b>AGILE</b> (<b>A</b>stro-rivelatore <b>G</b>amma a <b>I</b>mmagini <b>LE</b>ggero) satellite flight model, conducted in June/July 2006 at IABG test facility.</div> <div class="htmlview paragraph"> ...
Matteo Giacomazzo   +5 more
openaire   +1 more source

Structural Test Model – Thermal Balance Test of ATV

SAE Technical Paper Series, 2003
<div class="htmlview paragraph">The Automated Transfer Vehicle will provide ISS with reboost, attitude control functions, with water, gas and propellant and with dry cargo. It remains attached up to 6 months before a destructive reentry.</div> <div class="htmlview paragraph">In summer 2002, a Thermal Balance Test has been performed ...
P. Vincent   +4 more
openaire   +1 more source

Design and development of thermal test model of a micro‐satellite for thermal balance test

Aircraft Engineering and Aerospace Technology, 2008
PurposeThis paper seeks to provide an insight into the design and development of the thermal test model (TTM) of X‐Sat, a 120 kg class micro‐satellite, being developed at the Centre. This model was specifically constructed for carrying out a thermal balance test (TBT) in a 4 m diameter vertical thermal vacuum chamber.Design/methodology/approachThe ...
Gilbert Justin Jose Nesamani   +4 more
openaire   +1 more source

Geosyncronous imager thermal balance test and thermal model modification

SPIE Proceedings, 2014
The multi-channel scanning imager is one of the main payloads of a Geostationary earth orbit satellite of China, which observe multi spectrum from earth. Passive thermal control was applied to decrease temperature rise when solar intrusion at midnight, and heat compensation was made to decrease thermal fluctuation in one orbit.
Bingting Hu   +3 more
openaire   +1 more source

Thermal Balance Test of the TOPEX/Poseidon Satellite

SAE Technical Paper Series, 1992
<div class="htmlview paragraph">The TOPEX/Poseidon spacecraft is scheduled for launch in August 1992 aboard an Ariane 42P launch vehicle. The mission is a collaborative scientific venture between NASA and CNES. The primary objective is to perform precise measurements of the ocean surface topography by radar altimetry from a precision, circular ...
P. E. Cleveland, F. DeMauro
openaire   +1 more source

Thermal Balance Testing of the European Robotic Arm

SAE Technical Paper Series, 2000
<div class="htmlview paragraph">As part of the European contribution to the Russian segment of the International Space Station (ISS), the European Robotic Arm (ERA) is designed under contract of the European Space Agency by Fokker Space as the Prime contractor.
Jan Doornink   +3 more
openaire   +1 more source

Home - About - Disclaimer - Privacy