Results 121 to 130 of about 383,072 (432)

Influence of AP Particle Size on Burning Characteristics of HMX/AP Propellants Supplemented with Fe2O3

open access: yesPropellants, Explosives, Pyrotechnics, EarlyView.
ABSTRACT Nitramine propellants have attracted considerable attention in the domain of solid rockets and gun propulsion because of their energetic and smokeless features. Ammonium perchlorate (AP) is the widely used oxidizer in propellants owing to the excellent burning characteristics.
Makoto Kohga   +2 more
wiley   +1 more source

An Integrated Method for Microwave Absorption and External Thermal Flow Simulation in SAR Antenna Vacuum Thermal Tests

open access: yesSensors
The simulation of microwave absorption and external thermal flow is an essential aspect of the vacuum thermal testing process for Synthetic Aperture Radar (SAR) antenna.
Shangjie Pan   +4 more
doaj   +1 more source

Numerical Study of the Thermal Model on High Uniformity Temperature Test Platform

open access: yesMATEC Web of Conferences, 2019
The surface temperature uniformity of a test platform with an effective test area of 600 mm × 600 mm was numerically studied. The conductive heat transfer model for the test platform and the device under test (DUT) installed on the surface was ...
Wang Zijuan   +3 more
doaj   +1 more source

Proceedings of the Spacecraft Charging Technology Conference: Executive Summary [PDF]

open access: yes, 1977
Aerospace environments are reviewed in reference to spacecraft charging. Modelling, a theoretical scheme which can be used to describe the structure of the sheath around the spacecraft and to calculate the charging currents within, is discussed ...
Bunn, M. H.   +5 more
core   +1 more source

Combining Magnetic and Electric Sails for Interstellar Deceleration

open access: yes, 2016
The main benefit of an interstellar mission is to carry out in-situ measurements within a target star system. To allow for extended in-situ measurements, the spacecraft needs to be decelerated.
Hein, Andreas M., Perakis, Nikolaos
core   +3 more sources

Eigenstructure Assignment Based Controllers Applied to Flexible Spacecraft [PDF]

open access: yes, 2011
The objective of this paper is to evaluate the behaviour of a controller designed using a parametric Eigenstructure Assignment method and to evaluate its suitability for use in flexible spacecraft.
Aranda J.   +4 more
core   +2 more sources

Assessing forecast benefits of future constellations of microwave sounders on small satellites using an ensemble of data assimilations

open access: yesQuarterly Journal of the Royal Meteorological Society, EarlyView.
An ensemble of data assimilations method is employed to evaluate the impact of different potential future small‐satellite constellations carrying microwave‐sounding instruments to explore the optimal design of a constellation for global numerical weather prediction.
Katie Lean   +5 more
wiley   +1 more source

Spacecraft Assembly Process Bill of Material Construction Technology For Single-Piece Production

open access: yesMATEC Web of Conferences, 2017
For the spacecraft assembly Process Bill of Material (PBOM) traditional construction technology, the product assembly relationship, product assembly information are not visual for spacecraft assembly and integration department, leading to the manual PBOM
He Wen-xing, Chen Chang-yu, Liu Yu-gang
doaj   +1 more source

Unambiguous signal reconstruction for GEO-LEO bistatic SAR with azimuth multichannel

open access: yesThe Journal of Engineering, 2019
Spaceborne bistatic multichannel synthetic aperture radar (MC-SAR) system employed inclined geosynchronous Earth orbit (GEO) transmitter and low-Earth-orbit (LEO) receiver can provide fine spatial resolution and a vast area of surveillance, which ...
Yuekun Wang   +4 more
doaj   +1 more source

Apparatus and method of capturing an orbiting spacecraft [PDF]

open access: yes, 1987
Apparatus and a method of capturing an orbiting spacecraft by attaching a grapple fixture are discussed. A probe is inserted into an opening, such as a rocket nozzle, in the spacecraft until a stop on the prove mechanism contacts the spacecraft.
Gardner, Dale A., Harwell, William D.
core   +1 more source

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