2025-02-23T10:56:11-05:00 DEBUG: VuFindSearch\Backend\Solr\Connector: Query fl=%2A&wt=json&json.nl=arrarr&q=id%3A%22irk-123456789-95439%22&qt=morelikethis&rows=5
2025-02-23T10:56:11-05:00 DEBUG: VuFindSearch\Backend\Solr\Connector: => GET http://localhost:8983/solr/biblio/select?fl=%2A&wt=json&json.nl=arrarr&q=id%3A%22irk-123456789-95439%22&qt=morelikethis&rows=5
2025-02-23T10:56:11-05:00 DEBUG: VuFindSearch\Backend\Solr\Connector: <= 200 OK
2025-02-23T10:56:11-05:00 DEBUG: Deserialized SOLR response
Оптимальные перелеты космических аппаратов с двухрежимными двигателями
An optimization problem of the interplanetary transfer of spacecraft with biregime nuclear rocket engine is formulated. The transfer trajectory is forming owing to combination of parts of high and low engine thrust. An analysis of necessary conditions of optimality is carried out. The solution o...
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| Main Authors: | , |
|---|---|
| Format: | Article |
| Language: | Russian |
| Published: |
Інститут механіки ім. С.П. Тимошенка НАН України
2010
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| Series: | Прикладная механика |
| Online Access: | http://dspace.nbuv.gov.ua/handle/123456789/95439 |
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