Investigations to characterize multijunction solar cells in the stratosphere using low-cost balloon and communication technologies
The use of current balloon, control and communication technologies to test multi-junction solar cells in the stratosphere to achieve near AMO conditions has been investigated. The design criteria for the technologies are that they be reliable, low cost and readily available. Progress is reported on...
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creator | Bowe, G.A. Qianghua Wang Woodyard, J.R. Johnston, R.R. Brown, W.J. |
description | The use of current balloon, control and communication technologies to test multi-junction solar cells in the stratosphere to achieve near AMO conditions has been investigated. The design criteria for the technologies are that they be reliable, low cost and readily available. Progress is reported on a program to design, launch, fly and retrieve payloads dedicated to testing multi-junction solar cells. The system investigated includes a state-of-the-art multi-junction solar cell and two-axis suntracker that weighs less than one pound. Data acquisition is carried out with a module that employs programmable microprocessors, A/D converters, digital I/O lines, AX.25 encoding, GPS, and VHF, UHF and HF transmitters. One flight has been carried with a 1000 gram extensible helium balloon and payload that weighed under six pounds. During a flight that lasted about two hours, the balloon traveled to an altitude of 87,000 feet and data were downlinked. The payload was retrieved about 40 miles from the launch site. |
doi_str_mv | 10.1109/PVSC.2000.916136 |
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The design criteria for the technologies are that they be reliable, low cost and readily available. Progress is reported on a program to design, launch, fly and retrieve payloads dedicated to testing multi-junction solar cells. The system investigated includes a state-of-the-art multi-junction solar cell and two-axis suntracker that weighs less than one pound. Data acquisition is carried out with a module that employs programmable microprocessors, A/D converters, digital I/O lines, AX.25 encoding, GPS, and VHF, UHF and HF transmitters. One flight has been carried with a 1000 gram extensible helium balloon and payload that weighed under six pounds. During a flight that lasted about two hours, the balloon traveled to an altitude of 87,000 feet and data were downlinked. 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During a flight that lasted about two hours, the balloon traveled to an altitude of 87,000 feet and data were downlinked. The payload was retrieved about 40 miles from the launch site.</description><subject>Communication system control</subject><subject>Communications technology</subject><subject>Costs</subject><subject>Data acquisition</subject><subject>Encoding</subject><subject>Microprocessors</subject><subject>Payloads</subject><subject>Photovoltaic cells</subject><subject>Terrestrial atmosphere</subject><subject>Testing</subject><issn>0160-8371</issn><isbn>0780357728</isbn><isbn>9780780357723</isbn><fulltext>true</fulltext><rsrctype>book_chapter</rsrctype><creationdate>2000</creationdate><recordtype>book_chapter</recordtype><sourceid>6IE</sourceid><sourceid>RIE</sourceid><recordid>eNotkEtLAzEUhQMq2Fb34ip_YOpNMpPpLKX4KBQULG7LnfTOTEomKZOMokt_uY-6OovDdz44jF0JmAsB1c3z68tyLgFgXgktlD5hUygXoIqylItTNgGhIVuoUpyzaYx7AAlKiwn7Wvk3ism2mGzwkafATYcDmkSD_STejy7Z_ejNb81jcDhwQ85Fbj1PHfGYBkwhHjoaiI_R-pa78J6ZEBOv0bnwg6HfcRP6fvTW_Hl4ItP54EJrKV6wswZdpMv_nLHN_d1m-Zitnx5Wy9t11mrQWQFGN42RVCqJuUHZaF0JFFg1talkRViIXDdFnitSNRRU6lo2aHZQV7XJtZqx6-OsJaLtYbA9Dh_b41vqG2qrY00</recordid><startdate>2000</startdate><enddate>2000</enddate><creator>Bowe, G.A.</creator><creator>Qianghua Wang</creator><creator>Woodyard, J.R.</creator><creator>Johnston, R.R.</creator><creator>Brown, W.J.</creator><general>IEEE</general><scope>6IE</scope><scope>6IH</scope><scope>CBEJK</scope><scope>RIE</scope><scope>RIO</scope></search><sort><creationdate>2000</creationdate><title>Investigations to characterize multijunction solar cells in the stratosphere using low-cost balloon and communication technologies</title><author>Bowe, G.A. ; Qianghua Wang ; Woodyard, J.R. ; Johnston, R.R. ; Brown, W.J.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-g606-50c6ffc2e732a4ca2f6691a1a9fbc929ea5146f5443e3b05e76b2facd0b9bc463</frbrgroupid><rsrctype>book_chapters</rsrctype><prefilter>book_chapters</prefilter><language>eng</language><creationdate>2000</creationdate><topic>Communication system control</topic><topic>Communications technology</topic><topic>Costs</topic><topic>Data acquisition</topic><topic>Encoding</topic><topic>Microprocessors</topic><topic>Payloads</topic><topic>Photovoltaic cells</topic><topic>Terrestrial atmosphere</topic><topic>Testing</topic><toplevel>online_resources</toplevel><creatorcontrib>Bowe, G.A.</creatorcontrib><creatorcontrib>Qianghua Wang</creatorcontrib><creatorcontrib>Woodyard, J.R.</creatorcontrib><creatorcontrib>Johnston, R.R.</creatorcontrib><creatorcontrib>Brown, W.J.</creatorcontrib><collection>IEEE Electronic Library (IEL) Conference Proceedings</collection><collection>IEEE Proceedings Order Plan (POP) 1998-present by volume</collection><collection>IEEE Xplore All Conference Proceedings</collection><collection>IEEE Electronic Library (IEL)</collection><collection>IEEE Proceedings Order Plans (POP) 1998-present</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Bowe, G.A.</au><au>Qianghua Wang</au><au>Woodyard, J.R.</au><au>Johnston, R.R.</au><au>Brown, W.J.</au><format>book</format><genre>bookitem</genre><ristype>CHAP</ristype><atitle>Investigations to characterize multijunction solar cells in the stratosphere using low-cost balloon and communication technologies</atitle><btitle>Conference Record of the Twenty-Eighth IEEE Photovoltaic Specialists Conference - 2000 (Cat. No.00CH37036)</btitle><stitle>PVSC</stitle><date>2000</date><risdate>2000</risdate><spage>1328</spage><epage>1331</epage><pages>1328-1331</pages><issn>0160-8371</issn><isbn>0780357728</isbn><isbn>9780780357723</isbn><abstract>The use of current balloon, control and communication technologies to test multi-junction solar cells in the stratosphere to achieve near AMO conditions has been investigated. The design criteria for the technologies are that they be reliable, low cost and readily available. Progress is reported on a program to design, launch, fly and retrieve payloads dedicated to testing multi-junction solar cells. The system investigated includes a state-of-the-art multi-junction solar cell and two-axis suntracker that weighs less than one pound. Data acquisition is carried out with a module that employs programmable microprocessors, A/D converters, digital I/O lines, AX.25 encoding, GPS, and VHF, UHF and HF transmitters. One flight has been carried with a 1000 gram extensible helium balloon and payload that weighed under six pounds. During a flight that lasted about two hours, the balloon traveled to an altitude of 87,000 feet and data were downlinked. The payload was retrieved about 40 miles from the launch site.</abstract><pub>IEEE</pub><doi>10.1109/PVSC.2000.916136</doi><tpages>4</tpages></addata></record> |
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identifier | ISSN: 0160-8371 |
ispartof | Conference Record of the Twenty-Eighth IEEE Photovoltaic Specialists Conference - 2000 (Cat. No.00CH37036), 2000, p.1328-1331 |
issn | 0160-8371 |
language | eng |
recordid | cdi_ieee_primary_916136 |
source | IEEE Electronic Library (IEL) Conference Proceedings |
subjects | Communication system control Communications technology Costs Data acquisition Encoding Microprocessors Payloads Photovoltaic cells Terrestrial atmosphere Testing |
title | Investigations to characterize multijunction solar cells in the stratosphere using low-cost balloon and communication technologies |
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