Results 121 to 130 of about 10,741 (228)

A dynamic simulation approach to optimize thrust regulation in electric pump-fed rocket engines. [PDF]

Sci Rep
Li T, He H, Yu N, Sun X, Cai G.
europepmc   +1 more source

Project LOCOST: Laser or Chemical Hybrid Orbital Space Transport [PDF]

A potential mission in the late 1990s is the servicing of spacecraft assets located in GEO. The Geosynchronous Operations Support Center (GeoShack) will be supported by a space transfer vehicle based at the Space Station (SS).
Dixon, Alan, Kost, Alicia, Lampshire, Gregory, Larsen, Rob, Monahan, Bob, Wright, Geoff   +5 more
core   +1 more source

Estimating CO2 emissions due to present and future suborbital space tourism industry. [PDF]

PLoS One
Huang AM, Xu Y.
europepmc   +1 more source

Optimization of combustion organization scheme for pre-combustion chamber of pre-cooled engine. [PDF]

Sci Rep, 2023
Yu N, Jiao B, Zhou C, Han S, Li T, Shi H.   +5 more
europepmc   +1 more source

Combustor design and analysis using the Rocket Combustor Interactive Design (ROCCID) methodology [PDF]

The ROCket Combustor Interactive Design (ROCCID) Methodology is a newly developed, interactive computer code for the design and analysis of a liquid propellant rocket combustion chamber.
Klem, Mark D., Pieper, Jerry L., Walker, Richard E.   +2 more
core   +1 more source

Advances in Structural Reliability Analysis of Solid Propellant Grain: A Comprehensive Review. [PDF]

Polymers (Basel)
Tang C, Qiang H, Geng T, Wang X, Zhang F.   +4 more
europepmc   +1 more source

Intelligent Fault Diagnosis of Liquid Rocket Engine via Interpretable LSTM with Multisensory Data. [PDF]

Sensors (Basel), 2023
Zhang X, Hua X, Zhu J, Ma M.
europepmc   +1 more source

Experimental Study on the Evolution of Mechanical Properties and Their Mechanisms in a HTPB Propellant Under Fatigue Loading. [PDF]

Polymers (Basel)
Feng F, Chen X, Xu J, Zeng Y, Huang W, Dong J.   +5 more
europepmc   +1 more source

A rapid method for optimization of the rocket propulsion system for single-stage-to-orbit vehicles [PDF]

A rapid analytical method for the optimization of rocket propulsion systems is presented for a vertical take-off, horizontal landing, single-stage-to-orbit launch vehicle.
Eldred, C. H., Gordon, S. V.
core   +1 more source

A versatile low-cost data acquisition system for small rocket engine test bench. [PDF]

HardwareX
Netzel NA, Batista DS, Granziera F, Tosin MC.   +3 more
europepmc   +1 more source