Results 71 to 80 of about 1,875 (170)
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
Development and implementation of promising technologies in JSC EDB Fakel [PDF]
The enterprise is mastering a number of technologies for obtaining functional materials for monopropellant thruster and Hall-effect thruster. The article describes advances in the development of a catalyst for the decomposition of hydrazine with high ...
E. A. Bogdanova +2 more
doaj
The thermal decomposition of hydrogen peroxide (H2O2) as a promising green propellant was performed over free-noble metallic-based catalysts deposited on abundant supports.
Imane Remissa +5 more
doaj +1 more source
Characteristics of ignition delay of hypergolic ionic liquids combined with 1-amino-4-methylpiperazine. [PDF]
Shin KS, Jang HG, Park SH, Cho SJ.
europepmc +1 more source
A Multimode Propulsion System (MPS) is an innovative spacecraft thruster concept that integrates two or more propulsion modes sharing the same type of propellant.
Alessandro A. Quarta +2 more
doaj +1 more source
Numerical Study of Flow Boiling of ADN-Based Liquid Propellant in a Capillary. [PDF]
Liu X, Su G, Yao Z, Yan Z, Yu Y.
europepmc +1 more source
Cargo transfer vehicle RCS propellant contamination issues [PDF]
The purpose of this report is to address Cargo Transfer Vehicle (CTV) RCS contamination issues and contribute to the resources necessary to optimize the vehicle and propulsion systems required in the CTV of the National Launch System (NLS) Heavy Lift ...
Ballard, Richard O.
core +1 more source
Expanding the ADN-Based Monopropellant Thruster Family
The development of High Performance Green Propulsion (HPGP) was initiated with the goal of meeting the requirements for future satellite missions. The HPGP technology includes a storable monopropellant blend based on Ammonium DiNitramide (ADN) and a thruster with a high-temperature resistant thrust chamber and catalyst. After more than 10 years of R&D,
Anflo, K., Moore, S., Moog Inc., P.King
openaire +1 more source
In a worldwide scenario which sees an increasing number of small satellite launches, novel mission concepts may be unlocked providing the spacecrafts with the very precise and rapid maneuvering capability that electric thrusters cannot guarantee. In this
Sergio Cassese +5 more
doaj +1 more source
Experimental and analytical comparison of flowfields in a 110 N (25 lbf) H2/O2 rocket [PDF]
A gaseous hydrogen/gaseous oxygen 110 N (25 lbf) rocket was examined through the RPLUS code using the full Navier-Stokes equations with finite rate chemistry. Performance tests were conducted on the rocket in an altitude test facility.
Kim, Suk C. +3 more
core +1 more source

