Published 1968 | Version v1
Report Open

Spectrometer for cosmic and solar protons experiment S 72 aboard the satellite ESRO 2

  • 1. Commissariat a l'Energie Atomique, Saclay (France). Centre d'Etudes Nucleaires

Description

The authors describe an experiment designed for the spectrometry of charged particles, and intended for the european satellite ESRO II, the launch of which is planned for may 1968. The polar orbit of this satellite will enable the experiment to measure, depending on the geomagnetic latitude, either the energy of solar protons, or the spectrum of the protons of the internal Van Allen belt, or even the spectrum of the abundance of galactic nuclei whose charge is smaller than 6. The equipment is built in two parts: - 1) a sensor including a telescope of solid state detectors of large area (lithium drifted silicon) and the preamplifiers; - 2) an electronic unit including the amplifiers, the pulse height discriminators and the coincidence circuits, the analog-to-digital converter which encodes the energy loss of an incident particle in one of the detectors, the sealer for counting the flux of the particles, and the interface to the telemetry system of the satellite. The equipment weights 1350 grams, drains 350 mW and is designed for normal operation from -20 C to +50 C. After the discussion of the design principles and after the description of the circuits and the explanation of their operation, emphasis will be laid on how have been met the requirements specific to space electronics; lightness, low power drain, vibration strength, wide range of working temperatures and above all reliability. The modifications brought to the flight model F-2 after the failure of the launch of the model F-1 in may 1967 are also reported. (authors)

Availability note (English)

Available from INIS in electronic form

Abstract (French)

On decrit une experience de spectrometrie de particules chargees d'origine cosmique, destinee au satellite europeen ESRO II, dont le lancement est prevu en mai 1968. L'orbite de ce satellite etant polaire, l'experience doit permettre de mesurer suivant la latitude, soit le spectre d'energie des protons solaires, soit celui des protons de la couche interne de Van Allen, soit encore le spectre d'abondance des noyaux galactiques de charge inferieure a 6. L'appareil comprend deux parties: - une sonde comportant un telescope de detecteurs a jonctions en silicium (au lithium diffuse) de grande surface et les preamplificateurs; - un boitier electronique comprenant les amplificateurs, les circuits de discrimination d'amplitude et de coincidence, le convertisseur analogique-numerique qui permet le codage de la perte d'energie d'une particule incidente dans l'une des jonctions, l'echelle de comptage du flux des particules, et l'interface de liaison avec la telemesure du satellite. L'ensemble pese 1350 g, consomme 350 mW et fonctionne normalement de - 20 C a + 50 C. Apres l'expose de l'organisation de l'experience et apres la description des circuits et de leur fonctionnement, on insiste plus particulierement sur la facon dont ont ete respectes les imperatifs propres a l'electronique spatiale: legerete, faible consommation, tenue aux vibrations, large gamme de temperature de fonctionnement et fiabilite. On decrit egalement les modifications apportees au modele de vol F-2 apres l'echec du lancement du modele F-1 en mai 1967. (auteur)

Files

36002806.pdf

Files (1.5 MB)

Name Size Download all
md5:1f78cf631fc7a7dab402e7d99933cf2f
1.5 MB Preview Download

Additional details

Additional titles

Original title (French)
Spectrometre pour protons cosmiques et solaires experience S 72 embarquee a bord du satellite ESRO 2

Publishing Information

Imprint Pagination
[87 p.]
Report number
CEA-R--3700

Optional Information

Notes
6 refs.