Mechanical Compression Behaviour of "Green" Rocket Propellants [PDF]
Problemy Mechatroniki, 2023 The issues related to mechanical resistance of solid rocket propellants, which can appear during storage or handling of the launching system, are considered to directly influence the burning performance.
Florin M. DÎRLOMAN +5 more
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Aerodynamic Characteristics of Supersonic Rocket-Sled Involving Waverider Geometry
Applied Sciences, 2022 Rocket-sleds belong to a category of large-scale test platforms running on the ground which are mainly used for launching tests of weapon equipment and performance tests of airborne equipment.
Yuanyuan Yu +3 more
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Research on attitude control strategy of single engine failure in the first-stage flight phase of new generation launch vehicle [PDF]
MATEC Web of Conferences, 2021 The successful launching of the new generation of launch vehicle is of great practical significance to the development of China Space, and the cryogenic liquid engine commonly used in the launch vehicle has a certain probability of failures, which may ...
Liao Guorui, Liu Jinjie, Dou Tianheng
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Acquisition of the Flight Information Using the KSR-3 Agnetometer [PDF]
Journal of Astronomy and Space Sciences, 2003 The KSR-3 magnetometers consist of the fluxgate magnetometer (MAG/AIM) for acquiring the rocket flight attitude information, and the search-coil magnetometer (MAG/SIM) for the observation of the Earth's magnetic fluctuations.
Sun-Mi Kim +9 more
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Research and Development of Fault Diagnosis Methods for Liquid Rocket Engines
Aerospace, 2022 Currently, considerable efforts are being focused on the development of reusable rockets and smart rockets due to the heavy requirements of future next-generation aerospace transportation.
Tao Wang, Lin Ding, Huahuang Yu
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Atmospheric Flow at Alcantara Launch Center [PDF]
Journal of Aerospace Technology and Management, 2022 The Alcantara Launch Center (ALC) is the main Brazilian access to space. It is positioned over a complex terrain, and it has some important buildings for assembling, integration and launching activities, such as the Mobile Integration Tower.
Karine Klippel +5 more
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Dynamic simulation study on the impact of wind on the location of the explosion belt of rocket explosive device [PDF]
Zhihui kongzhi yu fangzhenIn this paper, aiming at the problem that the explosion belt is offset by wind during the operation of rocket explosive device, the dynamic model affected by wind and launching angle in different environments are established.
TU Jiangang, CHEN Shi, ZHANG Kaikai
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In situ measurements of sub-meter plasma waves over low-latitude ionosphere during Leonid-99 meteor storm [PDF]
Annales Geophysicae, 2004 In situ probe measurements of plasma parameters were carried out on 18 and 20 November 1999 from Sriharikota, India, a low-latitude rocket launching station to investigate the effect of a Leonid meteor storm.
S. P. Gupta, R. Sekar, Y. B. Acharya
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Rocket in situ observation of equatorial plasma irregularities in the region between E and F layers over Brazil [PDF]
Annales Geophysicae, 2017 A two-stage VS-30 Orion rocket was launched from the equatorial rocket launching station in Alcântara, Brazil, on 8 December 2012 soon after sunset (19:00 LT), carrying a Langmuir probe operating alternately in swept and constant bias modes.
S. Savio Odriozola +6 more
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Report of the Sounding Rocket Experiment at Syowa Station : 1970-1973
Antarctic Record, 1975 The rocket launching facilities were inaugurated in 1969 and completed in 1971 at Syowa Station (60°00'S, 39° 35'E: geomagnetic lat. 69.6°S, long. 77.1°E). In the rocket range, about 500 m south-west of the main base: of Syowa, there are three buildings,
Masaru AYUKAWA +3 more
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