Results 131 to 140 of about 32,742 (216)

Comprehensive Observations of Magnetospheric Particle Acceleration, Sources, and Sinks (COMPASS): A Mission Concept to Explore the Extremes of Jupiter's Magnetosphere. [PDF]

Space Sci Rev
Clark G, Kollmann P, Kinnison J, Kelly D, Haapala A, Li W, Jaynes AN, Blum L, Marshall R, Turner D, Cohen I, Ukhorskiy A, Mauk BH, Roussos E, Nénon Q, Drozdov A, Woodfield E, Dunn W, Berland G, Kraft R, Williams PKG, Smith HT, Hospodarsky G, Wu X, Hulsman J, O'Brien TP, Looper M, Sorathia K, Sciola A, Sicard A, Donegan M, Clare B, Emmell D, Wirzburger J, Sepulveda D, Roufberg L, Perry J, Schellhase J, Pergosky D, Able E, O'Neill M, Fernandes C, Chattopadhyay D, Bibelhauser S, Kijewski S, Pulkowski J, Furrow M, Feldman C, Nichols J, Carr N, Verma H, Lindsay S, Bunce E, Parry B, Martindale A.   +54 more
europepmc   +1 more source

INSPACE CHEMICAL PROPULSION SYSTEMS AT NASA's MARSHALL SPACE FLIGHT CENTER: HERITAGE AND CAPABILITIES [PDF]

NASA s Marshall Space Flight Center (MSFC) is well known for its contributions to large ascent propulsion systems such as the Saturn V rocket and the Space Shuttle external tank, solid rocket boosters, and main engines.
Blevins, J. A., McRight, P. S., Sheehy, J. A.   +2 more
core   +1 more source

Recent advances in bio-microsystem integration and Lab-on-PCB technology. [PDF]

Microsyst Nanoeng
Papamatthaiou S, Menelaou P, El Achab Oussallam B, Moschou D.   +3 more
europepmc   +1 more source

Design evolution of the orbiter reaction control subsystem [PDF]

The challenges of space shuttle orbiter reaction control subsystem development began with selection of the propellant for the subsystem. Various concepts were evaluated before the current Earth storable, bipropellant combination was selected.
Belvins, D., Henderson, J., Hohmann, C., Karakulko, W., Taeber, R. J.   +4 more
core   +1 more source

Study of auxiliary propulsion requirements for large space systems. Volume 1: Executive summary [PDF]

An insight into auxiliary propulsion systems (APS) requirements for large space systems (LSS) launchable by a single shuttle is presented. In an effort to scope the APS requirements for LSS, a set of generic LSSs were defined.
Machles, G. W., Smith, W. W.
core   +1 more source

The Pioneer Anomaly. [PDF]

Living Rev Relativ, 2010
Turyshev SG, Toth VT.
europepmc   +1 more source

Microfluidic Flame Barrier [PDF]

Propellants flow through specialized mechanical hardware that is designed for effective and safe ignition and sustained combustion of the propellants. By integrating a micro-fluidic porous media element between a propellant feed source and the combustion
Fisher, David J., Mungas, Christopher, Mungas, Gregory S.   +2 more
core   +1 more source

MONOPROPELLANT THRUSTERS FIRING TEST USING KC12GA CATALYST

MONOPROPELLANT THRUSTERS FIRING TEST USING KC12GA CATALYST
3rd European Workshop on Hydrazine(9 June 2004), Cagliari, Sardinia, Italy 資料番号: ARDS04034000 レポート番号: 2004ESASP.556E ...
openaire  

Study of a modular extravehicular activity work platform [PDF]

Configurations for extravehicular activity work platforms for astronaut use in orbital ...

core   +1 more source

Cryogenic propellant management in space: open challenges and perspectives. [PDF]

NPJ Microgravity
Simonini A, Dreyer M, Urbano A, Sanfedino F, Himeno T, Behruzi P, Avila M, Pinho J, Peveroni L, Gouriet JB.   +9 more
europepmc   +1 more source