Wyniki wyszukiwania - BazTech

1

Solid Rocket Boosters Separation System Development for the ILR-33 Amber 2K Rocket

Kierski Jan, Pazik Arthur, Cieśliński Dawid

Transactions on Aerospace Research

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2023

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Nr 3 (272)

16--27

EN

The paper presents the development process of the solid rocket boosters (SRBs) separation system of the ILR-33 AMBER 2K rocket. A redesign of the system was required due to the development of new, larger SRBs. The main system requirements were transmission of forces and moments between the SRBs and the main stage, execution of the separation process at a given moment in flight and mechanical integration simplification. A set of aerodynamics calculations were performed. With the use of computational fluid dynamics software, forces acting on the booster during separation for several angles of attack, as well as the critical booster deflection angle, have been determined. Next, a mathematical model was created to define the load spectrum acting on the system during the flight and separation phases, covering both static and dynamic loads. All the internal and external force sources were considered. A series of motion dynamics simulations were conducted for representative flight cases. Then, the system operational parameters were verified with the use of dedicated ground test facilities. Necessary calibrations of the mathematical model were then implemented, leading to a high level of confidence with the empirical data obtained, thereby leading to a successful system qualification for the flight campaign.

2

On the Safety of Suborbitalrocket Launches from the Polish Coast

Noga Tomasz, Matysek Krzysztof, Dziczkaniec Rafał, Cieśliński Dawid, Umiński Piotr, Dul Stanisław

Safety & Defense

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2023

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1

31--46

EN

This paper presents a rocket flight safety analysis using methods from the internationally recognized standard RCC 321-20 with an emphasis on a suborbital launch from the Polish coast. Currently, several entities are launching (or planning to launch) suborbital rockets and land them in the Baltic sea – and such flights are expected to be performed using more and more capable rockets with increasing launch frequency. While the present approach in Poland is to close a predefined air space, monitor or close the maritime zone to any traffic and ensure that the impact point dispersion of all rocket elements will fit within that restricted area, established and proven methods often take advantage of advanced calculations of flight risk to the public, aircraft and vessels. This paper demonstrates this approach and compares relative rocket or missile flight safety from Poland to other locations frequently used for such exercises. The results of this work may also be beneficial when planning safety measures for military exercises involving missiles.

3

High altitude ballooning as an atmospheric sounding system in the pre-flight procedures of ILR-33 Amber

Spiralski Marcin, Bęben Karol, Konior Wojciech, Cieśliński Dawid

Transactions on Aerospace Research

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2020

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Nr 1 (258)

66--77

EN

The paper presents research on the near real-time atmospheric sounding system. The main objective of the research was the development and testing of the weather sounding system based on a weather balloon. The system contains a redundant system of radiosondes, a lifting platform containing weather balloon and a holding system as well as ground station. Several tests of the system were performed in August and September 2019. Altitude, reliability, resistance to weather conditions and data convergence were tested. During tests, new procedures for such missions were developed. The final test was performed for the ILR-33 Amber Rocket as a part of pre-launch procedures. The test was successful and allowed to use acquired atmospheric data for further processing. Several post-tests conclusions were drawn. The altitude of sounding by a weather balloon depends mostly on weather conditions, the amount of gas pumped and the weight of a payload. The launching place and experience of the crew play an important role in the final success of the mission, as well.

PL

W artykule przedstawiono badania nad systemem sondowania atmosferyczny w czasie zbliżonym do rzeczywistego. Głównym celem badania było stworzenie oraz testowanie systemu sondowania atmosfery opartego o balony meteorologiczne. W skład systemu wchodzi redundantny system radiosond, platforma nośna zawierająca balon meteorologiczny i system mocujący, a także stacja naziemna. W sierpniu i wrześniu 2019 r. przeprowadzono kilka testów systemu. Badano wysokość, niezawodność, odporność na warunki atmosferyczne i zbieżność danych z innymi źródłami. Podczas testów opracowano nowe procedury dla misji tego typu. Końcowy test został przeprowadzony dla rakiety ILR-33 Bursztyn w ramach procedur przedstartowych. Test zakończył się sukcesem i umożliwił wykorzystanie pozyskanych danych atmosferycznych do dalszego przetworzenia. Wyciągnięto kilka wniosków po testowych. Wysokość sondowania osiągana przez balon meteorologiczny zależy głównie od warunków pogodowych, ilości wtłoczonego gazu i masy ładunku użytkowego. Miejsce startu i doświadczenie załogi odgrywają również ważną rolę w końcowym sukcesie misji.