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On the Safety of Suborbitalrocket Launches from the Polish Coast

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

Safety & Defense

2023

31--46

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.

Suborbital Rockets in Safety & Defense Applications

Noga Tomasz

Safety & Defense

2021

65--79

This paper presents benefits from using suborbital rockets in safety & defense applications. The paper describes suborbital rockets and their contribution to modern science, research and technology development. A historical view of suborbital rockets and their applications in safety & defense roles is discussed. Chosen research & development activities, military exercises and air defense systems’ tests performed using suborbital rockets in various countries are listed and described based on a literature review of publicly available sources. The paper presents capabilities of Łukasiewicz Research Network - Institute of Aviation in the field of suborbital rockets. A development of ILR-33 AMBER 2K rocket reaching flight speeds over Mach 4 and optimized to reach 100 km altitude is described with comment regarding its applicability in safety & defense applications supported by flight simulations.