Results 91 to 100 of about 3,658 (232)

Characteristics of ignition delay of hypergolic ionic liquids combined with 1-amino-4-methylpiperazine. [PDF]

RSC Adv, 2023
Shin KS, Jang HG, Park SH, Cho SJ.
europepmc   +1 more source

S-4B orbital workshop attitude control system study [PDF]

Saturn S-4B orbital workshop attitude control system ...
Bunyak, R. S., Curtis, H. S., Ewald, W. J.   +2 more
core   +1 more source

Experimental evaluation of high-thrust, throttleable, monopropellant hydrazine reactors [PDF]

Throttleable monopropellant hydrazine catalytic reactors of a size applicable to a planetary landing vehicle were designed, fabricated, and tested. An experimental evaluation of two 2670-N reactor designs was conducted.
Kruger, G. W., Riebling, R. W.
core   +1 more source

Life Cycle Sustainability Assessment of Monopropellant Propulsion Systems: Advancing the Comparison Between Conventional and Novel Monopropellants

IAF Space Transportation Solutions and Innovations Symposium
Within the field of monopropellant chemical propulsion, hydrazine has been the industry standard for over 50 years. During the past three decades, this has been challenged by the development and adoption of so-called novel monopropellants, which feature a lower propellant toxicity while delivering equal or improved performance compared to hydrazine ...
Deroo, Pepijn, Jyoti, Botchu, Wilson, Andrew   +2 more
openaire   +2 more sources

Cargo transfer vehicle RCS propellant contamination issues [PDF]

The purpose of this report is to address Cargo Transfer Vehicle (CTV) RCS contamination issues and contribute to the resources necessary to optimize the vehicle and propulsion systems required in the CTV of the National Launch System (NLS) Heavy Lift ...
Ballard, Richard O.
core   +1 more source

Firing Test Campaign for a Hydrogen Peroxide Propulsion System for CubeSats in Vacuum Conditions

Aerospace
This work reports the results of an on-ground experimental test campaign performed in the relevant environment (i.e., inside a vacuum chamber) of a blowdown H2O2 monopropellant propulsion system designed for CubeSat applications for the assessment of its
Angelo Pasini, Elia Puccinelli, Stefano Calatafimi, Carlos Muñoz Moya, Juliusz Saryczew, Thomas Searle   +5 more
doaj   +1 more source

High energy propellants - A continuing bibliography with indexes [PDF]

Bibliography on solid, liquid, and hybrid high energy propellants and oxidizers, propellant handling and storage, toxicity and hazards, and safety ...

core   +1 more source

Design and Analysis of a Micro–Electro-Mechanical System Thruster for Small Satellites and Low-Thrust Propulsion

Aerospace
As a cost-effective and versatile solution, small satellites are increasingly being considered for space exploration. However, one of the major challenges in deploying small satellites for high total impulse missions, particularly deep space exploration,
Yubin Zhong, Fabrizio Ponti, Francesco Barato, Guojun Xia, Siyu Li, Xiao Zhang, Tao Wu   +6 more
doaj   +1 more source

Combustion instability prediction using a nonlinear bipropellant vaporization model [PDF]

Combustion instability prediction using nonlinear bipropellant vaporization ...
Breen, B. P., Hoffman, R. J., Wright, R. O.   +2 more
core   +1 more source

Propulsion simulation for magnetically suspended wind tunnel models [PDF]

The feasibility of simulating propulsion-induced aerodynamic effects on scaled aircraft models in wind tunnels employing Magnetic Suspension and Balance Systems. The investigation concerned itself with techniques of generating exhaust jets of appropriate
Beerman, Henry P., Chen, James, Joshi, Prakash B., Krech, Robert H., Lintz, Andrew L., Rosen, David I.   +5 more
core   +1 more source