Abstrakti
The paper considers the usage of proton exchange membrane fuel cells, gaseous H2 and cryogenic H2 fuels to solve the known thermal problems associated with electrical generation. Recent experimental H2 flight failures are reviewed, and a novel solution to control the electrolyte temperature operating range is proposed, utilising LH2, new additive manufactured evaporators/ heat exchangers and control software.
The need for an IRON BIRD full scale test rig is justified prior to any further ambitious flight attempts.
The need for an IRON BIRD full scale test rig is justified prior to any further ambitious flight attempts.
Alkuperäiskieli | Englanti |
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Otsikko | 33rd Congress of the International Council of the Aeronautical Sciences ICAS2022 |
Alaotsikko | Conference Proceedings |
Kustantaja | The International Council of the Aeronautical Sciences |
Tila | Julkaistu - 4 syysk. 2022 |
OKM-julkaisutyyppi | A4 Artikkeli konferenssijulkaisussa |
Tapahtuma | Congress of the International Council of the Aeronautical Sciences - Stockholm, Ruotsi Kesto: 4 syysk. 2022 → 9 syysk. 2022 |
Julkaisusarja
Nimi | ICAS Legal Notes |
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ISSN (elektroninen) | 2958-4647 |
Conference
Conference | Congress of the International Council of the Aeronautical Sciences |
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Maa/Alue | Ruotsi |
Kaupunki | Stockholm |
Ajanjakso | 4/09/22 → 9/09/22 |
Julkaisufoorumi-taso
- Jufo-taso 0