Electronically Driven Combustion of Energetic Ionic Liquids in a Microcell Reactor. [PDF]
ACS OmegaHauck C +5 more
europepmc +1 more source
Soft Ferrofluid Actuator Based on 3D-Printed Scaffold Removal. [PDF]
3D Print Addit Manuf, 2021 Shabaniverki S +3 more
europepmc +1 more source
Valve, normally closed, titanium Pyronetics model 1426 [PDF]
Performance tests of the explosive actuated, normally closed titanium valve 1426, are outlined. The valves are used to control hydrazine flow in a monopropellant thruster. Data cover pressure tests, internal and external leakage tests, flow control tests,
Avalos, E.
core +1 more source
Research progress on the catalytic and thermal decomposition of ammonium dinitramide (ADN). [PDF]
RSC AdvTian Y +8 more
europepmc +1 more source
Cerium oxide based active catalyst for hydroxylammonium nitrate (HAN) fueled monopropellant thrusters. [PDF]
RSC Adv, 2018 Agnihotri R, Oommen C.
europepmc +1 more source
Overview of the Main Propulsion System for a Nuclear Thermal Propulsion Flight Demonstrator [PDF]
A demonstration of a Nuclear Thermal Propulsion (NTP) engine has not been conducted in over 50 years. Several tests were conducted during the NERVA program but no NTP engine was ever flown in space. In the last several years there has been a considerable
Bean, Q. A. +2 more
core +1 more source
Ionic Liquid-Based Gas Generators Using High Voltage Nanosecond Pulse Discharge. [PDF]
ACS OmegaHauck C +5 more
europepmc +1 more source
Handbook of recommended practices for the determination of liquid monopropellant rocket engine performance [PDF]
The design, installation, and operation of systems to be used for directly measuring quantities of fundamental importance to the determination of monopropellant thruster performance is described. Areas covered include: (1) force and impulse measurement; (
Baerwald, R. K. +2 more
core +1 more source
Civilian mass exposure to hydrazine after an F-16 crash: a retrospective descriptive study. [PDF]
BMC Emerg MedUcar AB, Demir H, Akoglu H.
europepmc +1 more source
Comparison study of exhaust plume impingement effects of small mono- and bipropellant thrusters using parallelized DSMC method. [PDF]
PLoS One, 2017 Lee KH.
europepmc +1 more source