Refine Your Search

Search Results

Author:
Viewing 1 to 3 of 3
Technical Paper

Evaluation of Mission Electromagnetic Irradiation with ESABASE/SUNLIGHT

1994-06-01
941352
ESABASE/SUNLIGHT is a software tool to calculate illumination, effective illumination, exposure time, incident electromagnetic power, absorbed electromagnetic energy for spacecraft surfaces during planet orbiting missions considering sun and planet irradiation, effects of eclipse and self-shading, multireflections, transmission, pointing and (variable) geometry. Calculation applies a fast Monte Carlo raytracing algorithm and is based on wavelength dependent spectra and material properties. ESABASE/SUNLIGHT is fully integrated in the CAE-frame ESABASE which offers a powerful geometry specification language, orbit generator, pointing facility and advanced libraries as well as gateway, pre-, postprocessing and display tools with the benefits of standardisation and exchange to other analysis tools.
Technical Paper

ESARAD Recent Improvements; a User's Viewpoint

1994-06-01
941563
The ESARAD radiative analysis program has been in use in the European thermal analysis community for approximately two years. The first part of this paper presents an assessment of ESARAD from a user's viewpoint. The second part presents work related to ESARAD performed in the Thermal Control and Life Support Division of ESTEC. In particular, work relating to two topics is presented: 1) ESARAD programming - a set of add-on software routines developed to complement ESARAD's basic capabilities is presented. 2) ESARAD applications - two thermal analysis problems from the ENVISAT - 1 and XMM spacecraft are presented. The last part of the paper is a brief description of the status of accuracy control in ESARAD.
Technical Paper

ABLAT, Ablation Modeling Extension to ESATAN

1992-07-01
921294
This paper discusses the capabilities of the ABLAT software which has been developed by ERC and Dornier for the European Space Agency. The software provides an ablation modelling capability for the ESATAN thermal analyser and consists of two sections: i. A stand-alone preprocessor allowing specification of the ablation model. This has both an X11/OSF Motif and a command line interface. ii. An integrated solver capability within the ESATAN system, allowing transient analysis of an ablating surface in conjunction with a standard thermal model. After a brief overview of the major aims of the development, the software is discussed from two main points of view, the user interface facilities (how the user defines the model to the system), and the calculation facilities (what can be calculated, and how are these calculations performed).
X