Error by ODEs solution - Help please - Mensajes
WroteWrote
Thanks, Alvaro!
My email OchkovVF@mpei.ru
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Wrote3 stages variation.
Checking with Tsiolkovsky rocket equation in a gravitational field with several stages
Alvaro.
There is such a Meshchersky equation. In the West it is called differently.
Уравнение Мещерского

В отношении И.В. Мещерского память потомков совершила вопиющую несправедливость. Дифференциальное уравнение движения тела переменной массы, которое И.В. Мещерский вывел и опубликовал ещё в 1897 году, спустя 31 год (!) было (по незнанию трудов Мещерского) заново выведено итальянским математиком Туллио Леви-Чивита. К сожалению, как это уже не раз бывало, о русском первооткрывателе на Западе забыли, и это уравнение стали называть "уравнением Леви-Чивита". (https://borisgen.livejournal.com/22811.html)
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Polet na Lunu.docx (496,8 KiB) descargado 931 vez(es).
Rakete-1.sm (17,75 KiB) descargado 1504 vez(es).
Rakete-2.sm (17,14 KiB) descargado 1512 vez(es).


WroteNew versions
Polet na Lunu.docx (496,8 KiB) descargado 931 vez(es).
Rakete-1.sm (17,75 KiB) descargado 1504 vez(es).
Rakete-2.sm (17,14 KiB) descargado 1512 vez(es).
Three examples: the napkin calculation of "Nine Days of One Year", a single-stage and a two-stage rocket with parameters such that humans could survive the flight (limited acceleration).
The first section of the pdf is based on Valery's text posted earlier. It also includes some tasks for the reader.
Rakete.sm (23,7 KiB) descargado 1555 vez(es).
Rakete2.sm (24,72 KiB) descargado 1520 vez(es).
Serviette.sm (9,43 KiB) descargado 1506 vez(es).
Rocket.pdf (421,58 KiB) descargado 1058 vez(es).
The first section of the pdf is based on Valery's text posted earlier. It also includes some tasks for the reader.
Rakete.sm (23,7 KiB) descargado 1555 vez(es).
Rakete2.sm (24,72 KiB) descargado 1520 vez(es).
Serviette.sm (9,43 KiB) descargado 1506 vez(es).
Rocket.pdf (421,58 KiB) descargado 1058 vez(es).
Technische Mechanik mit SMath Studio: https://link.springer.com/book/10.1007/978-3-658-50592-9
Whether m(t) is P or P+m[2 after engine cut-off depends on whether you get rid of the structure of the second stage or not. As long as we don't consider any subsequent maneuvers, the difference has no influence. If you do nothing, then payload and empty second stage will orbit side by side, separated or not.
Technische Mechanik mit SMath Studio: https://link.springer.com/book/10.1007/978-3-658-50592-9
WroteWhether m(t) is P or P+m[2 after engine cut-off depends on whether you get rid of the structure of the second stage or not. As long as we don't consider any subsequent maneuvers, the difference has no influence. If you do nothing, then payload and empty second stage will orbit side by side, separated or not.
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