Bibliografie tematiche / Raketit

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  1. Articoli di riviste
  2. Tesi
  3. Libri
  4. Capitoli di libri
  5. Atti di convegni

Letteratura scientifica selezionata sul tema "Raketit"

Autore: Grafiati
Pubblicato: 29 luglio 2024
Ultima modifica: 30 luglio 2024

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Articoli di riviste sul tema "Raketit"

1

Lukman, Moh. "Perencanaan Peningkatan Kualitas Produk Raket dengan Metode Quality Function Deployment". Jurnal Teknik Industri 10, n. 1 (22 febbraio 2010): 44. http://dx.doi.org/10.22219/jtiumm.vol10.no1.44-51.

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Small Industry Abadi location in central small industry raket Sukun-Malang, so many kinds racket product are many variables as, racket quality, raket colors, rakets price, will give the customer many choice product rackets. Demand racket products are fluctuative from periods to another periods because there are factors: school holiday, and badminton championship in scale national cup and world cup as All England so demand will be increase. In central small industry raket thre are many small industry racket, so competition raket product increase,so there are the price will be cheap and quality may be too lower. This competition cause qoitition in raket "X" is low. Antisipacition to win competition we will design good quality raket product fit with attribute racket customers, with methode Quality Function Deployment (QFD). From result of analysis can know that attribute obtaining especial priority to customer is among others chicken eye of strong plastic type and handle of racket is not breakable, besides technical respon which made account of by company is among others wrap handle of sponge cloth and of racket don't use extension T. Besides got by price for new desain equal to Rp19.300,- at the price of selling Rp22.500,- got by cheaper price of Rp1.300,- compared to old desain racket that is equal to Rp20.600,- at the price of selling Rp25.000.
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Nábrády, Mária. "Az érzelmek szocializációjának tranzakcióanalitikus megközelítése. A rakett érzések hatása az érzelemfelismerésre preadoleszcens korban". Magyar Pszichológiai Szemle 57, n. 2 (1 settembre 2002): 251–88. http://dx.doi.org/10.1556/mpszle.57.2002.2.1.

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A tanulmány áttekinti a rakett érzés tranzakcióanalitikus koncepcióját, mely a rakett érzést úgy határozza meg, mint egy másik, autentikus érzést helyettesíto, tanult érzést. Az autentikus érzés megjelenése a stresszhelyzetekben adekvát lenne, de a szocializáció során szülei elutasítása nyomán a személy megtanulta elnyomni és más elfogadott érzéssel helyettesíteni azt. A fogalmat a hasonló jelenségeket megragadó egyéb érzelemelméletek fogalmaival vetjük össze. A tanulmány célja: (1) a rakett érzés mérésére használható módszert adni és (2) megvizsgálni, hogyan hat a rakett érzés az érzelemfelismerésben mutatkozó perceptuális torzítás irányára. E célból két tesztet szerkesztettünk a rakett érzések és az érzelemfelismerés mérésére. Ezeket egy IQ-teszttel együtt 142 (11-14 éves) személlyel vettük fel. Az eredmények azt mutatják, hogy az érzelemfelismerés pontossága pozitív kapcsolatban van az álta­lános intelligenciával, és bizonyos rakett érzések esetén (szégyen, irigység, szánalom, zavar) az érze­lem-felismerési feladatokban ezen érzések felé perceptuális torzítás történik.
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Dick, Alexander. "SCHWEDISCHE RAKETE". Opernwelt 63, n. 4 (2022): 46. http://dx.doi.org/10.5771/0030-3690-2022-4-046.

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Greiner, Bernd. "Die Logik der Raketen". Zeitschrift für Ideengeschichte 6, n. 3 (2012): 5–18. http://dx.doi.org/10.17104/1863-8937-2012-3-5.

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Steinmüller, Peter. "Rampenstart mit Rakete". VDI nachrichten 74, n. 30-31 (2020): 26. http://dx.doi.org/10.51202/0042-1758-2020-30-31-26-2.

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Mayer, Hans W. "Mit Raketen-Fritz auf Rekordjagd". VDI nachrichten 75, n. 37 (2021): 26. http://dx.doi.org/10.51202/0042-1758-2021-37-26.

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Dikić, Goran. "Problem pouzdanosti protivoklopnih raketnih sistema". Vojnotehnicki glasnik 40, n. 5 (1992): 39–44. http://dx.doi.org/10.5937/vojtehg9201039d.

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Holler, Marcel. "Raumfahrt: Feste Treibstoffe für Raketen". Nachrichten aus der Chemie 71, n. 5 (28 aprile 2023): 22–25. http://dx.doi.org/10.1002/nadc.20234135674.

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Jung, Frank. "Von Zeppelinen, Raketen und Autoschiffen". ATZ - Automobiltechnische Zeitschrift 125, n. 7-8 (luglio 2023): 10–13. http://dx.doi.org/10.1007/s35148-023-1622-4.

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Nadya, Maulita, e Lisa Sulisyawati. "Probabilitas Konsumen Membeli Raket Li-Ning Terhadap Pesaing Raket Yonex Berdasarkan Aspek Citra Merek, Harga dan Kualitas Produk (Studi pada Toko Raket Murah Surabaya)". Jurnal Disrupsi Bisnis 4, n. 3 (20 maggio 2021): 252. http://dx.doi.org/10.32493/drb.v4i3.10484.

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Abstract (sommario):
Probabiltas adalah suatu ukuran tentang kemungkinan suatu peristiwa akan terjadi dimasa yang akan datang. Li-Ning dan Yonex merupakan merek raket yang terkenal di kalangan pecinta olahraga Bulutangkis, yang dibedakan oleh label. Penelitian ini bertujuan untuk mengetahui probabilitas marjinal raket Li-Ning dan raket Yonex, probabilitas bersama raket Li-Ning dan raket Yonex dan probabilitas bersyarat raket Li-Ning terhadap pesaing raket Yonex berdasarkan aspek citra merek, harga dan kualitas produk. Jenis metode penelitian adalah kuantitatif. Teknik sampel yaitu sampling kuota dan sampling purposive. Teknik analisis data adalah analisa probabilitas. Ditinjau dari hasil probabilitas marjinal, disimpulkan bahwa probabilitas tertinggi adalah probabilitas konsumen membeli raket Li-Ning dan raket Yonex karena kualitas produk sebesar 0,80. Ditinjau dari probabilitas bersama konsumen raket Li-Ning disimpulkan bahwa probabilitas tertinggi adalah probabilitas konsumen yang membeli raket Li-Ning karena kualitas produk sebesar 0,96. Sedangkan konsumen raket Yonex, bahwa probabilitas tertinggi adalah probabilitas yang membeli raket Yonex karena citra merek yaitu sebesar 0,74. Jika ditinjau dari probabilitas bersyarat, disimpulkan bahwa probabilitas tertinggi adalah probabilitas raket Li-Ning terhadap pesaing raket Yonex karena kualitas produk sebesar 0,96. Keywords: Probabilitas; Citra Merek; Harga; Kualitas Produk; Keputusan Konsumen
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Tesi sul tema "Raketit"

1

Thorsell, Johanna. "Raketen - Skolbibliotekarie, elev och lärare i samverkan för ökad informationskompetens". Thesis, Uppsala University, Department of ALM, 2008. http://urn.kb.se/resolve?urn=urn:nbn:se:uu:diva-101867.

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Musil, Tomáš. "Létající atmosférický nosič pro vypouštění raket". Master's thesis, Vysoké učení technické v Brně. Fakulta strojního inženýrství, 2021. http://www.nusl.cz/ntk/nusl-443187.

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Abstract (sommario):
The main objective of this thesis is to introduce the reader to the problematics of air-launch and to a custom design solution applying this concept. The specifics of this method of bringing a payload into orbit are described and explained. Overview of projects which use aircraft to launch spacecraft is included. Determination of primary parameters of a launch vehicle designed to carry a payload of a specified mass is conducted. The required flight performance has been estimated, a computational model has been developed in software MATLAB, and a multidisciplinary optimization of the design parameters has been performed using a genetic algorithm optimization method. Parameters of the designed air-launched rocket are compared with those of a ground-launched rocket. According to the specific criteria, the Airbus A310-300 aircraft was selected as the most suitable transport aircraft to be used for launching the designed launch vehicle. The last part of the thesis is devoted to the proposal of necessary modifications and estimation of the flight performance.
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Furvall, Frida, e Ingrid Ruotimaa. "- Som en raket! : Digitaliserad matematikundervisning i förskolan". Thesis, Luleå tekniska universitet, Institutionen för hälsa, lärande och teknik, 2021. http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-85221.

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Abstract (sommario):
Denna studie handlar om hur förskollärare kan iscensätta en matematikundervisning med hjälp av digitala verktyg på ett enkelt och roligt sätt. Läroplanen för förskolan Lpfö 18 anger att barnen ska få möjlighet att utveckla digital kompetens samt att utbildningen ska vara rolig och lärorik (Skolverket, 2018). Vi vill med denna studie bidra med kunskap om hur ett tvärvetenskapligt arbetssätt kan genomföras med hjälp av Bishops matematiska aktivitet design samt genom urskiljning och variation. Metoden som vi har använt i denna studie är att vi har genomfört en digitaliserad matematikundervisning med hjälp av variationsteorin och med inspiration från learning study. Undervisningen var inspirerad av barnprogrammet Supersagan där barnen genom den matematiska aktiviteten designa fick erfara de geometriska formerna samt att vi fick möjlighet till att berika vår profession. Resultatet visar att en undervisning med fokus på design kan bidra till ett matematiskt lärande för barn när förskolläraren riktar barnens uppmärksamhet mot lärandeobjektet och dess kritiska aspekter, visar på likheter och skillnader samt ger barnen tillgång till de rätta matematiska begreppen. Resultatet visar även att barns uttryck för matematik synliggörs genom deras förklaringar både verbalt och icke verbalt, deras tidigare erfarenheter samt att matematik uttrycks spontant i lek.
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Andersson, Cecilia. "Rådjur och raketer : gatukonst som estetisk produktion och kreativ praktik i det offentliga rummet /". Stockholm : HLS förlag, 2006. http://urn.kb.se/resolve?urn=urn:nbn:se:su:diva-1314.

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Andersson, Cecilia. "Rådjur och raketer : Gatukonst som estetisk produktion och kreativ praktik i det offentliga rummet". Doctoral thesis, Stockholms universitet, Institutionen för undervisningsprocesser, kommunikation och lärande (UKL), 2006. http://urn.kb.se/resolve?urn=urn:nbn:se:su:diva-1314.

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The purpose of this thesis is to describe and analyse the visual expressions of Street Art that occurs in the public space, and by doing so, to study this specifi c practice, and also elucidate the relation between public space as a democratic idea, a place for freedom of speech and as a planned, aesthetically shaped place. The intention is to throw light upon a central part of many young peoples lives in a didactic aspect. In this thesis I discuss Street Art as an informal image making in public space that young people use as tools to make meaning, but also as a form of resistance. The methodologies used in the study are ethnography and visual ethnography, where observational studies of Street Art as practice, interviews and interpretation of photographs (my own, and my informants) are performed and analysed. Theoretically, the study has a didactic and semiotic approach but I also rely on Cultural Studies as a research fi eld in order to be able to pick up different kinds of theories. From three platforms; public space and public place and places for Street Art, aesthetic learning processes within this specifi c practice, and fi nally the expanded fi eld of Art and the similarities and differences between formal Art and Street Art I have outlined four themes; ephemerality, the criteria for Street Art practice, how the work is being done, as a collective and individual practice, the struggle of space in public space, and fi nally high and low in Art and culture. By describing and analysing this informal image making light is thrown upon the aesthetic learning process that occurs, the didactic aspect of this practice and the communication that the images articulate. As a result, the study shows that Street Art, in spite of its illegal mark, points out that it is an aesthetic production and a creative practice that consists of resistance, meaning making, achieving knowledge through practice, and above all a way to use the city, to become a part of the city. The thesis contributes with the suggestion that this informal aesthetic learning process is a way to form identity, make meaning, take part of public space, and through symbolic resistance demand ones rights of expression.
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6

Markl, Albert Walter. "An initial guess generator for launch and reentry vehicle trajectory optimization". [S.l. : s.n.], 2001. http://www.bsz-bw.de/cgi-bin/xvms.cgi?SWB9578197.

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Rakette, Sonja [Verfasser], e Thilo [Akademischer Betreuer] Stehle. "Structural Analysis of Serine/Threonine Protein Kinase B and Multiple Peptide Resistant Factor of Staphylococcus aureus / Sonja Rakette ; Betreuer: Thilo Stehle". Tübingen : Universitätsbibliothek Tübingen, 2013. http://d-nb.info/1162843691/34.

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Bruzelius, Nils. ""Near friendly or neutral shores" : the deployment of the fleet ballistic missile submarines and US policy towards Scandinavia, 1957-1963 /". Stockholm : Avd. för teknik- och vetenskapshistoria, Kungliga Tekniska högskolan, 2007. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-4308.

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Ghadiani, Saeed Reza. "A multiphasic continuum mechanical model for design investigations of an effusion-cooled rocket thrust chamber". Köln : Deutsches Zentrum für Luft- und Raumfahrt e. V, 2005. http://www.gbv.de/dms/goettingen/508838495.pdf.

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Rakete, Stefan [Verfasser], Marcus A. [Akademischer Betreuer] Glomb e Mirko [Akademischer Betreuer] Bunzel. "Aufklärung molekularer Mechanismen beim Abbau von Dextrinen und Hopfenbittersäuren im Zuge der Bieralterung : [kumulative Dissertation] / Stefan Rakete. Betreuer: Marcus A. Glomb ; Mirko Bunzel". Halle, Saale : Universitäts- und Landesbibliothek Sachsen-Anhalt, 2014. http://nbn-resolving.de/urn:nbn:de:gbv:3:4-13013.

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Libri sul tema "Raketit"

1

Lagerstedt, Ilpo. Rakettimiehiä: Kilpajuoksu kuuhun. Hämeenlinna: Karisto, 2008.

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Chertok, B. E. Rakety i li︠u︡di: Ot samoletov do raket. Moskva: RTSoft, 2006.

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Mishin, Vasiliĭ Pavlovich. Ot sozdanii︠a︡ ballisticheskikh raket k raketno-kosmicheskomu mashinostroenii︠u︡. Moskva: Informat︠s︡ionno-izdatelʹskiĭ t︠s︡entr "Inform-Znanie", 1998.

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Ioĭrȳsh, A. I. Raketȳ dolzhnȳ sluzhit' miru: Iz istorii poyavleniya raketno-yadernogo oruzhiya. Moskva: Mezhdunarodnȳe otnosheniya, 1985.

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Kuznet︠s︡ov, N. P. Utilizat︠s︡ii︠a︡ raket s ZhRD: (na primere rakety 8K14). Moskva: Reguli︠a︡rnai︠a︡ i khaoticheskai︠a︡ dinamika, 2004.

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Ioĭrysh, Abram Isaakovich. Rakety dolzhny sluzhitʹ miru: Iz istorii poi͡a︡vlenii͡a︡ raketno-i͡a︡dernogo oruzhii͡a︡. Moskva: "Mezhdunar. otnoshenii͡a︡", 1985.

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Aleichem, Sholem. Sipure rakevet. Tel Aviv: Devir, 1989.

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Aviram, Ram. Rakevet taḥtit. Tel-Aviv: Zemorah-Bitan, 1997.

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Angelevich, A. E. Pervye raketki. Moskva: Intergraf Servis, 1995.

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Aviram, Ram. Rakevet taḥtit. Tel-Aviv: Zemorah-Bitan, 1997.

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Capitoli di libri sul tema "Raketit"

1

Messerschmid, Ernst, e Stefanos Fasoulas. "Thermische Raketen". In Raumfahrtsysteme, 169–228. Berlin, Heidelberg: Springer Berlin Heidelberg, 2000. http://dx.doi.org/10.1007/978-3-662-09674-1_5.

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Messerschmid, Ernst, e Stefanos Fasoulas. "Thermische Raketen". In Raumfahrtsysteme, 181–240. Berlin, Heidelberg: Springer Berlin Heidelberg, 2017. http://dx.doi.org/10.1007/978-3-662-49638-1_5.

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Messerschmid, Ernst, e Stefanos Fasoulas. "Thermische Raketen". In Raumfahrtsysteme, 185–244. Berlin, Heidelberg: Springer Berlin Heidelberg, 2010. http://dx.doi.org/10.1007/978-3-642-12817-2_5.

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Eversberg, Thomas. "Russen, Raketen und Wahlkampf". In Hollywood im Weltall, 5–16. Berlin, Heidelberg: Springer Berlin Heidelberg, 2013. http://dx.doi.org/10.1007/978-3-8274-3022-9_2.

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Wagner, Hermann Th, Klaus Jürgen Fischer e Joachim-Dietrich von Frommann. "Gasturbinen (Raketen- und Strahltriebwerke)". In Strömungs- und Kolbenmaschinen, 361–89. Wiesbaden: Vieweg+Teubner Verlag, 1986. http://dx.doi.org/10.1007/978-3-663-13921-8_16.

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Wagner, Hermann Th, Klaus Jürgen Fischer e Joachim-Dietrich von Frommann. "Gasturbinen (Raketen- und Strahltriebwerke)". In Strömungs- und Kolbenmaschinen, 361–89. Wiesbaden: Vieweg+Teubner Verlag, 1990. http://dx.doi.org/10.1007/978-3-663-13922-5_16.

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Wagner, Hermann Th, Klaus Jürgen Fischer e Joachim-Dietrich von Frommann. "Gasturbinen (Raketen- und Strahltriebwerke)". In Strömungs- und Kolbenmaschinen, 363–91. Wiesbaden: Vieweg+Teubner Verlag, 1993. http://dx.doi.org/10.1007/978-3-663-07750-3_16.

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Piper, Sven. "Aktuelle Raketen und zukünftige Trägersysteme". In Space – Die Zukunft liegt im All, 53–75. Berlin, Heidelberg: Springer Berlin Heidelberg, 2019. http://dx.doi.org/10.1007/978-3-662-59004-1_4.

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Seboldt, Wolfgang. "Ignition! – Missionskonzepte, fiktive Raketen und Antriebssysteme". In Expedition ins Sternenmeer, 139–53. Berlin, Heidelberg: Springer Berlin Heidelberg, 2022. http://dx.doi.org/10.1007/978-3-662-63730-2_8.

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Piper, Sven. "Erratum zu: Aktuelle Raketen und zukünftige Trägersysteme". In Space – Die Zukunft liegt im All, E1. Berlin, Heidelberg: Springer Berlin Heidelberg, 2019. http://dx.doi.org/10.1007/978-3-662-59004-1_11.

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Atti di convegni sul tema "Raketit"

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Avila Diaz, Mario, Thomas Yechout e Elaine Bryant. "'The Rakelet' - A Wingtip Modification Approach to Improve Endurance, Range and Fuel Savings". In 50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2012. http://dx.doi.org/10.2514/6.2012-669.

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Arianto, Ivan Setia, Nuri Nuri, Mahardika Prasetya Aji e Sulhadi Sulhadi. "ANALISIS TARIKAN DAN DIAMETER SENAR RAKET BADMINTON TERHADAP PANTULAN SHUTTLECOCK". In SEMINAR NASIONAL FISIKA 2016 UNJ. Pendidikan Fisika dan Fisika FMIPA UNJ, 2016. http://dx.doi.org/10.21009/0305020210.

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Miščič, Valter. "Vzpostavitev podatkovne baze iz pogorišča". In OTS 2023 Sodobne informacijske tehnologije in storitve. Univerza v Mariboru, Univerzitetna založba, 2023. http://dx.doi.org/10.18690/um.feri.8.2023.22.

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Vse pogostejše in obsežnejše naravne in tudi drugim katastrofe spremljajo naše življenje v zadnjem obdobju. Obsežni požari, povodnji in potresi uničujejo naša mesta, rakete uničujejo infrastrukturo. Ogrožena so naša življenja, premoženje in vse, kar smo ustvarjali desetletja in kar nam je najvažnejše in najdražje. Če pogledamo na te stvari iz oči naših podjetij, so najpomembnejša stvar prav gotovo njeni podatki. Firma, ki zgubi svoje najpomembnejše podatke, praktično izgubi vse. Firme se morajo na takšne dogodke pripraviti in svoje podatke ustrezno zaščititi. S podvojevanjem računskih centrov vključno z vso strojno in programsko opremo ter podatki se lahko dokaj dobro zaščitimo. Žal, vse firme nimajo tega privilegija. Dodatni računski center seveda stane in pri denarju se največkrat ustavi. Velikokrat pa gre zgolj za nezavedanje ali podcenjevanje te problematike. Vsekakor je dobro, da imamo pripravljen načrt okrevanja, da mu vsi sledimo in da neprestano vadimo postopke okrevanja.
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Sirac oğlu Süleymanov, Mehman. "44 GÜNLÜK VƏTƏN MÜHARİBƏSİNİN DÖYÜŞ TAKTİKASINA GƏTİRDİYİ YENİLİKLƏR". In VII REPUBLICAN CONFERENCE OF SCIENTIFIC SOURCES. https://aem.az/, 2022. http://dx.doi.org/10.36719/2663-4619/2022/03/07/6-10.

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Açar sözlər: döyüş taktikası, pilotsuz uçuş aparatları, əks-hücum, döyüş hədəfi, hərb tarixi Key words: combat tactics, unmanned aerial vehicles, counter-attack, combat target, military history 2020-ci il sentyabr ayının 27-də başlayan və böyük Zəfərlə tamamlanan 44 günlük müharibənin çox mühüm nəticələrindən biri də onun dünya döyüş taktikasına böyük yeniliklər gətirməsi oldu. Bu yeniliklər döyüşlərin aparılması taktikası ilə bağlı mövcud olan təsəvvürlərdə bir çevriliş etdi ki, indi onlar dünyanın güclü ordularının rəhbərləri və hərb mütəxəssisləri tərəfindən maraqla öyrənilməkdədir. Həmin yeniliklər ilk növbədə pilotsuz uçuş aparatlarının kütləvi və səmərəli tətbiqi ilə bağlıdır. Azərbaycanın pilotsuz uçuş aparatlarının səmərəli istifadəsi ilə erməni tanklarının və digər texnikanın hələ döyüş xəttinə gəlib çatmamış, cəbhənin dərinliklərində məhv edilməsi görüntüləri ən müxtəlif hərbi mütəxəssislərdə inanılası mümkün olmayan bir şok effekti yaratmışdı. Hətta Azərbaycan tərəfindən erməni hədəflərinin kütləvi şəkildə məhv edilməsi ilə bağlı nümayiş etdirilən görüntüləri bəzi amerikalı ekspertlər informasiya müharibəsinin elementləri kimi qəbul edirdilər. Azərbaycan təcrübəsinin reallığını qəbul edən mütəxəssislər isə hesab edirdilər ki, Amerikanın İrak VII Respublika Elmi Qaynaqlar Konfransının Materialları / 4 may 2022 Materials of the VII Republican Conference of Scientific Sources / 4 May 2022 DOI: https://www.doi.org/10.36719/2663-4619/2022/03/07 7 müharibəsində raket-artilleriya sistemlərinin fəaliyyəti ilə bombalama şoku yaratmaq təcrübəsi artıq köhnəlmiş taktikadır (1).
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Kobald, M., C. Schmierer, U. Fischer, K. Tomilin, A. Petrarolo e M. Rehberger. "The HyEnD stern hybrid sounding rocket project". In Progress in Propulsion Physics – Volume 11. Les Ulis, France: EDP Sciences, 2019. http://dx.doi.org/10.1051/eucass/201911025.

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The student team Hybrid Engine Development (HyEnD) of the University of Stuttgart is taking part with the Institute of Space Systems (IRS) in the DLR educational program STERN (Studentische Experimentalraketen). This program supports students at German universities to design, build, and launch an experimental rocket within a 3-year project time frame. HyEnD is developing a hybrid rocket called HEROS (Hybrid Experimental Rocket Stuttgart) with a design thrust of 10 kN, a total impulse of over 100 kN·s, and an expected liftoff weight up to 175 kg. HEROS is planned to be launched in October 2015 from Esrange in Sweden to an expected flight altitude of 40 to 50 km. The current altitude record for amateur rockets in Europe is at approximately 21 km. The propulsion system of HEROS is called HyRES (Hybrid Rocket Engine Stuttgart) and uses a paraffin-based solid fuel and nitrous oxide (N2O) as a liquid oxidizer. The development and the test campaign of HyRES is described in detail. The main goals of the test campaign are to achieve a combustion efficiency higher than 90% and provide stable operation with low combustion chamber pressure fluctuations. The successful design and testing of the HyRES engine was enabled by the evaluation and characterization of a small-scale demonstrator engine. The 500-newton hybrid rocket engine, called MIRAS (MIcro RAkete Stuttgart), has also been developed in the course of the STERN project as a technology demonstrator. During this test campaign, a ballistic characterization of paraffin-based hybrid rocket fuels with different additives in combination with N2O and a performance evaluation were carried out. A wide range of operating conditions, fuel compositions, injector geometries, and engine configurations were evaluated with this engine. Effects of different injector geometries and postcombustion chamber designs on the engine performance were analyzed. Additionally, the appearance of combustion instabilities under certain conditions, their effects, and possible mitigation techniques were also investigated. Concluding, the development and construction of an advanced, lightweight hybrid sounding rocket for the given requirements and budget within the DLR STERN program are described herein. The most important parts include a high thrust hybrid rocket engine, the development of a light weight oxidizer tank, pyrotechnical valves, carbon fiber rocket structure, recovery systems, and onboard electronics.
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