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undergraduate thesis
Algoritam analize pogonskih parametara raketnog pogona
2012. urn:nbn:hr:235:441610
Karlić, Damir
University of Zagreb
Faculty of Mechanical Engineering and Naval Architecture

Cite this document

Karlić, D. (2012). Algoritam analize pogonskih parametara raketnog pogona (Undergraduate thesis). Zagreb: University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture. Retrieved from https://urn.nsk.hr/urn:nbn:hr:235:441610

Karlić, Damir. "Algoritam analize pogonskih parametara raketnog pogona." Undergraduate thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, 2012. https://urn.nsk.hr/urn:nbn:hr:235:441610

Karlić, Damir. "Algoritam analize pogonskih parametara raketnog pogona." Undergraduate thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, 2012. https://urn.nsk.hr/urn:nbn:hr:235:441610

Karlić, D. (2012). 'Algoritam analize pogonskih parametara raketnog pogona', Undergraduate thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, accessed 05 April 2025, https://urn.nsk.hr/urn:nbn:hr:235:441610

Karlić D. Algoritam analize pogonskih parametara raketnog pogona [Undergraduate thesis]. Zagreb: University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture; 2012 [cited 2025 April 05] Available at: https://urn.nsk.hr/urn:nbn:hr:235:441610

D. Karlić, "Algoritam analize pogonskih parametara raketnog pogona", Undergraduate thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, Zagreb, 2012. Available at: https://urn.nsk.hr/urn:nbn:hr:235:441610

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Metadata
TitleAlgoritam analize pogonskih parametara raketnog pogona
Title (english)The algorithm for analyzes operating parameters of missile propulsion
AuthorDamir Karlić
MentorBranimir Matijašević (mentor)
GranterUniversity of Zagreb
Faculty of Mechanical Engineering and Naval Architecture
Zagreb
Defense date and country2012-02-17, Croatia
Scientific / art field,
discipline and subdiscipline		TECHNICAL SCIENCES
Mechanical Engineering
Abstract
U završnom radu su analizirani karakteristični parametri raketnog pogona u uvijetima njegova rada, tj. u uvijetima koji vladiaju pri lansiranju i vertikalnom uzdizanju rakete. U radu su prikazane jednadžabe potiska rakete, maksimalnog potiska rakete, stvarnog potiska malaznice i jednadžebe specifičnog impulsa za faze uzdizanja rakete, odnosno prikazana je promjena brzine rakete pri vertikalnom letu. Prikazane su i osnovne karakteristike krutih i tekućih goriva i data je teoretska osnova rada raketnog motora i njegov kratak opis. Karakteristični parametri su prikazani za promijenjive i stacionarne uvjete u letu prilikom uzdizanja rakete, pri čemu su navedene jednadžbe prikazane u općem smislu i za konkretan slučaj rakete Saturn V, pomoću odgovarajućih numeričkih vrijednosti i grafičkih prikaza.
Keywords
Languagecroatian
URN:NBNurn:nbn:hr:235:441610
Study programmeTitle: Aeronautical Studies
Study programme type: university
Study level: undergraduate
Academic / professional title: sveučilišni/a prvostupnik/ prvostupnica (baccalaureus/baccalaurea) inženjer/inženjerka zrakoplovnog inženjerstva (sveučilišni/a prvostupnik/ prvostupnica (baccalaureus/baccalaurea) inženjer/inženjerka zrakoplovnog inženjerstva)
Type of resourceText
File originBorn digital
Access conditionsAccess restricted to students and staff of home institution
Terms of useLicence In copyright icon
Created on2019-05-22 00:50:56