Numerical comparison of exhaust plume flow behaviors of small monopropellant and bipropellant thrusters. [PDF]
PLoS One, 2017 Lee KH.
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. +2 more
core +1 more source
Cerium oxide based active catalyst for hydroxylammonium nitrate (HAN) fueled monopropellant thrusters. [PDF]
RSC Adv, 2018 Agnihotri R, Oommen C.
europepmc +1 more source
Comparison study of exhaust plume impingement effects of small mono- and bipropellant thrusters using parallelized DSMC method. [PDF]
PLoS One, 2017 Lee KH.
europepmc +1 more source
Ionic Liquid-Based Gas Generators Using High Voltage Nanosecond Pulse Discharge. [PDF]
ACS OmegaHauck C +5 more
europepmc +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
OSIRIS-REx Contamination Control Strategy and Implementation. [PDF]
Space Sci Rev, 2018 Dworkin JP +61 more
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
Research progress on the catalytic and thermal decomposition of ammonium dinitramide (ADN). [PDF]
RSC AdvTian Y +8 more
europepmc +1 more source