Mass and power modeling of communication satellites [PDF]
Analytic estimating relationships for the mass and power requirements for major satellite subsystems are described. The model for each subsystem is keyed to the performance drivers and system requirements that influence their selection and use ...
Pidgeon, David +2 more
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Propulsion simulation for magnetically suspended wind tunnel models [PDF]
The feasibility of simulating propulsion-induced aerodynamic effects on scaled aircraft models in wind tunnels employing Magnetic Suspension and Balance Systems. The investigation concerned itself with techniques of generating exhaust jets of appropriate
Beerman, Henry P. +5 more
core +1 more source
AerospaceThis paper presents a mission concept for a Low Earth Orbit (LEO) satellite equipped with a payload for space experiments, designed to be recovered on Earth post-mission.
Antonio Sannino +5 more
doaj +1 more source
Preparation and Performance Evaluation of Platinum Barium Hexaaluminate Catalyst for Green Propellant Hydroxylamine Nitrate Thrusters. [PDF]
Materials (Basel), 2021 Kang S, Kwon S.
europepmc +1 more source
Spark-integrated propellant injector head with flashback barrier [PDF]
, 2012 High performance propellants flow through specialized mechanical hardware that allows for effective and safe thermal decomposition and/or combustion of the propellants.
Fisher, David James +2 more
core +1 more source
Characteristics of ignition delay of hypergolic ionic liquids combined with 1-amino-4-methylpiperazine. [PDF]
RSC Adv, 2023 Shin KS, Jang HG, Park SH, Cho SJ.
europepmc +1 more source
TOPEX satellite option study [PDF]
The basic design of the fleet satellite communication spacecraft (FLTSATCOM) can easily accommodate any of the three payload options for the ocean dynamic topography experiment (TOPEX).
core +1 more source
Numerical Study of Flow Boiling of ADN-Based Liquid Propellant in a Capillary. [PDF]
Materials (Basel), 2023 Liu X, Su G, Yao Z, Yan Z, Yu Y.
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
Development and implementation of promising technologies in JSC EDB Fakel [PDF]
Космические аппараты и технологииThe 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