Strain MS2379T was isolated from a pasteurized solution sample from a predominantly anaerobic fermentation system processing bovine manure in Pilot Point, Texas. Phylogenetic analyses based on both 16S rRNA gene and rpoB gene sequences showed that MS2379T was most closely related to Paenibacillus polymyxa (DSM 36T), P. jamilae (DSM 13815T), and P. peoriae (DSM 8320T), yet DNA–DNA relatedness through DNA–DNA hybridization revealed only 22.6, 32.0 and 24.7 % relatedness to these three species respectively. Rod-shaped cells of strain MS2379T are Gram-stain variable with sub-terminal, ellipsoidal, deforming endospores. The peptidoglycan contains meso-diaminopimelic acid (mDAP) and the predominant fatty acids are anteiso-C15 : 0 (61.9 %) and anteiso-C17 : 0 (11.6 %), confirming that strain MS2379T has diagnostic features of other Paenibacillus species. The G+C content of MS2379T is 45.9 mol%. Fermentation of glucose yields acid and gas end-products. The polar lipids found were diphosphatidylglycerol, phosphatidylglycerol, phosphatidylethanolamine, and glycolipids, but also included some unidentified lipids, aminolipids, aminoglycolipid, and phosphatidylmethylethanolamine. The growth range of MS2379T was observed from 10–45 °C with optimal growth temperature at 30 °C. Growth was observed between pH 6–10 and up to 3 % NaCl. Unlike the most closely related Paenibacillus species, strain MS2379T was negative in the Voges-Proskauer reaction. Nucleic acid, chemotaxonomic and biochemical features support the distinctiveness of strain MS2379T. Thus, strain MS2379T represents a novel species of the genus Paenibacillus for which the name Paenibacillus ottowii sp. nov. is proposed with the type strain MS2379T (=DSM 107750T=ATCC TSD-165T).

The influence of electromagnetic induction coil launcher (EICL) system parameters on the launch performance was analyzed, and a method for measuring the launch performance of an EICL system with a muzzle velocity and energy conversion efficiency was proposed. The EICL system mainly includes a pulse power supply and launcher. The parameters of the pulse power supply mainly include the discharge voltage and the capacitance value of the capacitor bank. The structural parameters of the launcher mainly include the bore size of the launcher, the air gap length between the armature and the drive coil, the length and width of the drive coil, and the trigger position of the armature. Change in single or multiple parameters in the launch system will influence the launch performance. The influence of single or multiple parameters on the launch performance was summarized, and the physical law as analyzed. The influence law of the EICL system parameters on the launch performance was obtained, which lays a theoretical foundation for the optimization design of EICL. Finally, experimental verification was carried out by a single-stage test platform.

Electromagnetic coil launcher is a kind of special linear motor. In order to study the trigger principles of multi‐stage electromagnetic coil launcher, based on the electromagnetic field theory, the paper deduced the field‐circuit coupling magnetic field control equations of multi‐stage synchronous inductive coil with the consideration of inter‐stage coupling, and analyzed the distribution law of magnetic lines of force, air‐gap magnetic field and current density for multi‐stage electromagnetic coil launcher. The following conclusions were reached: the largest part of magnetic flux was at the intermediate stages of multi‐stage electromagnetic coil launcher; each stage of drive coil compensates for the magnetic field of the upper coil, thus making a stable air‐gap magnetic field; the induced current density was mainly distributed in the tail and surface of the armature; according to anti‐electromagnetic shock design principle of multi‐stage electromagnetic coil launcher (namely, the requirement for small fluctuation of electromagnetic force), the basic principle of multistage trigger was summarized, that is the principle of keeping air‐gap magnetic field and induced current constant. Thus, the design foundation was laid for the operation of multistage electromagnetic coil launcher. © 2021 Institute of Electrical Engineers of Japan. Published by Wiley Periodicals LLC.

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