Results 121 to 130 of about 1,875 (170)

Multimodal electrospray thruster for small spacecraft: design and experimental characterization. [PDF]

J Elect Propuls
Mallalieu P, Jugroot M.
europepmc   +1 more source

Study of a modular extravehicular activity work platform [PDF]

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

core   +1 more source

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

Ion propulsion cost effectivity [PDF]

Ion propulsion modules employing 8-cm thrusters and 30-cm thrusters were studied for Multimission Modular Spacecraft (MMS) applications. Recurring and nonrecurring cost elements were generated for these modules.
Biess, J. J., Zafran, S.
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

Green Propellant Infusion Mission Program Development and Technology Maturation [PDF]

The NASA Space Technology Mission Directorate's (STMD) Green Propellant Infusion Mission (GPIM) Technology Demonstration Mission (TDM) is comprised of a cross-cutting team of domestic spacecraft propulsion and storable green propellant technology experts.
Aggarwal, Pravin K., Bacha, Caitlin E., Bury, Kristen, Cardiff, Eric H., Deans, Matthew, Deininger, William D., Joniatis, John, Martinez, Jonathan, McLean, Christopher H., Spores, Ronald A., Yim, John T.   +10 more
core   +1 more source

AF-M315E Propulsion System Advances and Improvements [PDF]

Even as for the GR-1 awaits its first on-orbit demonstration on the planned 2017 launch of NASA's Green Propulsion Infusion Mission (GPIM) program, ongoing efforts continue to advance the technical state-of-the-art through improvements in the performance,
Allen, May, Arrington, Lynn A., Driscoll, Elizabeth, Masse, Robert K., Schneider, Steven J., Spores, Ronald A., Vasek, Thomas E.   +6 more
core   +1 more source

Effcts of Catalysts on Hydrazine Monopropellant Thruster Performance

Effcts of Catalysts on Hydrazine Monopropellant Thruster Performance
資料番号 ...
openaire  

The Pioneer Anomaly. [PDF]

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