Atmospheric Reentry Demonstrator balloon flight test

1999 ◽  
Vol 36 (4) ◽  
pp. 507-510 ◽  
Author(s):  
Maurizio De Giorgis ◽  
Giorgio Borriello ◽  
Andrea Allasio ◽  
Raffaele Vavala ◽  
Thierry Leveugle ◽  
...  
Keyword(s):  
Flight Test ◽  
Balloon Flight ◽  
Atmospheric Reentry

High Altitude Balloon Flight Test of the GRAD Experiment

1990 ◽  
Author(s):  
Robert J. Hicks ◽  
David H. Jenkins
Keyword(s):  
High Altitude ◽  
Flight Test ◽  
Balloon Flight

scholarly journals Balloon flight test of a CeBr3 detector with silicon photomultiplier readout

2021 ◽  
Author(s):  
David Murphy ◽  
Joseph Mangan ◽  
Alexei Ulyanov ◽  
Sarah Walsh ◽  
Rachel Dunwoody ◽  
...  
Keyword(s):  
Integrated Circuit ◽  
Gamma Ray ◽  
Pressure Sensors ◽  
Flight Test ◽  
Space Environment ◽  
Raspberry Pi ◽  
Balloon Flight ◽  
Silicon Photomultiplier ◽  
Near Space ◽  
Future Space

AbstractRecent advances in silicon photomultiplier (SiPM) technology and new scintillator materials allow for the creation of compact high-performance gamma-ray detectors which can be deployed on small low-cost satellites. A small number of such satellites can provide full sky coverage and complement, or in some cases replace the existing gamma-ray missions in detection of transient gamma-ray events. The aim of this study is to test gamma-ray detection using a novel commercially available CeBr3 scintillator combined with SiPM readout in a near-space environment and inform further technology development for a future space mission. A prototype gamma-ray detector was built using a CeBr3 scintillator and an array of 16 J-Series SiPMs by ON Semiconductor. SiPM readout was performed using SIPHRA, a radiation-tolerant low-power integrated circuit developed by IDEAS. The detector was flown as a piggyback payload on the Advanced Scintillator Compton Telescope balloon flight from Columbia Scientific Balloon Facility. The payload included the detector, a Raspberry Pi on-board computer, a custom power supply board, temperature and pressure sensors, a Global Navigation Satellite System receiver and a satellite modem. The balloon delivered the detector to 37 km altitude where its detection capabilities and readout were tested in the radiation-intense near-space environment. The detector demonstrated continuous operation during the 8-hour flight and after the landing. It performed spectral measurements in an energy range of 100 keV to 8 MeV and observed the 511 keV gamma-ray line arising from positron annihilation in the atmosphere with full width half maximum of 6.8%. During ascent and descent, the detector count rate peaked at an altitude of 16 km corresponding to the point of maximum radiation intensity in the atmosphere. Despite several engineering issues discovered after the flight test, the results of this study confirm the feasibility of using CeBr3 scintillator, SiPMs, and SIPHRA in future space missions.

Mars Balloon Flight Test Results

2009 ◽  
Author(s):  
Jeffery Hall ◽  
Michael Pauken ◽  
Viktor Kerzhanovich ◽  
Gerald Walsh ◽  
Eric Kulczycki ◽  
...  
Keyword(s):  
Flight Test ◽  
Test Results ◽  
Balloon Flight

Gondola performances, launch, recovery and facilities qualification for Atmospheric Demonstrator balloon flight test

1997 ◽  
Author(s):  
O. Cosentino ◽  
M. Falvella ◽  
A. Leonardi ◽  
D. Spoto ◽  
E. Morelli ◽  
...  
Keyword(s):  
Flight Test ◽  
Balloon Flight

Atmospheric reentry flight test of winged space vehicle

1992 ◽  
Author(s):  
YOSHIFUMI INATANI ◽  
RYOJIRO AKIBA ◽  
MOTOKI HINADA ◽  
MAKOTO NAGATOMO
Keyword(s):  
Space Vehicle ◽  
Flight Test ◽  
Atmospheric Reentry
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