In addition, the PVP incineration is technologically relevant in ceramic sintering [8], ceramic sensor fabrication [8, 9], battery electrode fabrication [6], waste destruction [10, 11], solid propellant development [12, 13], etc.
Argon is being used as a propellant in the development of the Variable Specific Impulse Magnetoplasma Rocket (VASIMR).
Between 1870 and 1890 much work was done on the development of propellants and explosives.
Although Unilever, who make most of the deodorants sold in Australia, have stated there is no technical solution on the horizon, they may well be the only ones with the research and development capacity to develop a safer propellant.
In October 1968 Malina gave a speech at JPL in which he highlighted Parsons' contribution to the U.S. rocket project, and lamented how it had come to be neglected, crediting him for making "key contributions to the development of storable propellants and of long duration solid propellant agents that play such an important role in American and European space technology".
While this tactic was vitiated by the development of smokeless propellant, the threat from more capable torpedo craft (later including submarines) remained.
In this work we describe the development of a propellant-based, portable oral inhalation platform for the pulmonary delivery of genes.
This study investigates the effects of the addition of metal-based high-energy matter (Aluminum) into the content of the propellant produced within the scope of development project.
In the development of a cryogenic propellant tank, the proper selection of adhesives to bond the composite and liner is important for the safety of operation.
An in-space propellant depot not only requires technology development in key areas such as zero boil-off storage and fluid transfer, but in other areas such as lightweight structures, highly reliable connectors, and autonomous operations.
The special attention given for motor case with 2 mm shell thickness, development of a slow burn rate propellant, ignition strategies for the slow burn rate propellant, stable burning of the low burn rate propellant and flow separation related issues for ground test are highlighted.
