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Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.

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At least 685 records · Page 38

Theory of plasma contactors for electrodynamic tethered satellite systems

Recent data from ground and space experiments indicate that plasma releases from an object dramatically reduce the sheath impedance between the object and the ambient plasma surrounding it. Available data is in qualitative accord with the theory developed to quantify the flow of current in the sheath. Electron transport in the theory is based on a fluid model of a collisionless plasma with an effective collision frequency comparable to frequencies of plasma oscillations. The theory leads to low effective impedances varying inversely with the square root of the injected plasma density. To support such a low impedance mode of operation using an argon plasma source, for example, requires that only one argon ion be injected for each thirty electrons extracted from the ambient plasma. The required plasma flow rates are quite low; to extract one ampere of electron current requires a mass flow rate of about one gram of argon per day.

Parks, D. E.↗

Plasma contactor design for electrodynamic tether applications

The plasma contacting process is described and experiments are discussed that suggest the key role that cold ions play in establishing a low impedance plasma bridge that can conduct current in either direction between a contactor electrode and a dilute plasma. A ring cusp contactor is shown to provide from 1000-mA of electron emission to 500-mA of electron collection as its bias relative to a simulated space plasma is varied through an 80-v range.

Wilbur, Paul J.↗

Studies of the lower thermosphere using a tethered satellite

Investigation of a proposed facility and review of the Atmosphere Explorer C (AE-C) satellite experience is presented. In order to properly take advantage of plans to operate in the lower thermosphere, it is necessary to have some foreknowledge of the natural environment in this region, how vehicles interact with the natural environment, and how instruments must be designed and built to operate in this environment. Some of the fundamental questions to be addressed by such a mission are reviewed as well as the AE-C satellite experience.

Torr, Marsha R.↗

Transient and steady inertially tethered clouds of gas in a vacuum

The generation, formation, and dissipation of a transient cloud of gas produced by a multiorifice ring jet are experimentally studied, and the results are compared to a long-term steady-state flow. The transient case is related to the steady-state case by comparison of their respective number density distributions in the flowfield. The shapes of the clouds are also observed and compared to the shape of the theoretical collisionless cloud. The results indicate that the steady-state cloud is concentrated into a smaller volume than the transient cloud, which tends to spread out farther radially as well as upstream. These differences seem to indicate that a surprisingly long time is required to attain steady flow, which may be due to a long-term buildup of collision products.

Farnham, Tony L.↗

Effects of neutral gas releases on electron beam injection from electrically tethered spacecraft

The presence of high neutral densities at low altitudes and/or during thruster firings is known to modify the spacecraft potential during active electron beam injection. Two-dimensional (three velocity) particle simulations are used to investigate the ionization processes including the neutral density required, the modification of the spacecraft potential, beam profile and spatial distribution of the return current into the spacecraft. Three processes are identified: (1) beam-induced ionization, (2) vehicle-induced ionization, and (3) beam plasma discharge. Only in the first two cases does the beam propagate away with little distortion.

Winglee, R. M.↗

Tethered variable gravity laboratory study: Low gravity process identification report

Experiments are described performable in the variable gravity environment, and the related compatible/beneficial residual accelerations, both for pure and applied research in the fields of Fluid Mechanics (static and dynamic), Materials Sciences (Crystal Growth, Metal and Alloy Solidification, Glasses, etc.), and Life Sciences, so as to assess the relevance of a variable G-level laboratory.

Briccarello, M.↗

Tethered gravity laboratories study

Variable Gravity Laboratory studies are discussed. The following subject areas are covered: (1) conceptual design and engineering analysis; (2) control strategies (fast crawling maneuvers, main perturbations and their effect upon the acceleration level); and (3) technology requirements.

Lucchetti, F.↗

Tethered gravity laboratories study

The following subject areas are covered: (1) thermal control issues; (2) attitude control sybsystem; (3) configuration constraints; (4) payload; (5) acceleration requirements on Variable Gravity Laboratory (VGL); and (6) VGL configuration highlights.

Lucchetti, F.↗

Stability analysis and control of tethered satellites

Issues of stability and stabilization of the Shuttle/Tethered Satellite System (TSS) are considered. The basic, nonlinear equations of motion of the TSS are derived using the system Lagrangian. A tension control strategy in feedback form is introduced to stabilize the TSS during station-keeping. In addition, the stability properties of a constant angle control method for deployment and retrieval are investigated using Liapunov stability theory.

Liaw, D.-C.↗