Mercury Propulsion is an undergraduate engineering team whose members hold different majors as offered from the College of Engineering at Embry-Riddle Aeronautical University in Prescott, Arizona. The team is tasked to design, build, instrument, and test a liquid rocket engine utilizing an optional Ejector Thrust Augmentation System (ETAS). The engine will burn liquid oxygen and ethanol as its propellants and be designed to produce 200 lb of thrust without augmentation. The end goal of the project is to produce thrust data from two five-second hot-fire tests; one with and one without the ETAS installed. Ignite Grant Awar
The Center for Space Exploration and Technology Research (cSETR) at The University of Texas at El Pa...
Amateur rocketry consists largely of rockets powered by solid propellant grains. The rocket industry...
Design and performance of liquid oxygen-liquid hydrogen thrust chamber for M-1 engin
The goal of this project is to design the University of Akron’s first design team built liquid propu...
The development of liquid oxygen/liquid methane (LOX/LCH4) propulsion systems has recently become a ...
The ERAU H2O flow project is developing a test stand which can be used to research the flow characte...
This work presents a preliminary design of a liquid rocket engine test platform to support research ...
The rapid growth in demand for spacecraft technologies has spawned a need for a variety of new and i...
The rapid growth in demand for spacecraft technologies has spawned a need for a variety of new and i...
The Eagle Space Flight Team was created with the goal of becoming the first undergraduate team to de...
Projects include: Liquids Division: Two research liquid engines one producing 500 pounds(Project Aqu...
Hybrid rockets, employed by companies like space tourism provider Virgin Galactic, use propellants t...
Under NASA Glenn Research Center sponsorship, MIT has developed the concept of micromachined, biprop...
Project Juno is a modular, liquid bi-propellant rocket engine being developed to serve as an experim...
The development of liquid oxygen/liquid methane (LOX/LCH4) propulsion systems has recently become a ...
The Center for Space Exploration and Technology Research (cSETR) at The University of Texas at El Pa...
Amateur rocketry consists largely of rockets powered by solid propellant grains. The rocket industry...
Design and performance of liquid oxygen-liquid hydrogen thrust chamber for M-1 engin
The goal of this project is to design the University of Akron’s first design team built liquid propu...
The development of liquid oxygen/liquid methane (LOX/LCH4) propulsion systems has recently become a ...
The ERAU H2O flow project is developing a test stand which can be used to research the flow characte...
This work presents a preliminary design of a liquid rocket engine test platform to support research ...
The rapid growth in demand for spacecraft technologies has spawned a need for a variety of new and i...
The rapid growth in demand for spacecraft technologies has spawned a need for a variety of new and i...
The Eagle Space Flight Team was created with the goal of becoming the first undergraduate team to de...
Projects include: Liquids Division: Two research liquid engines one producing 500 pounds(Project Aqu...
Hybrid rockets, employed by companies like space tourism provider Virgin Galactic, use propellants t...
Under NASA Glenn Research Center sponsorship, MIT has developed the concept of micromachined, biprop...
Project Juno is a modular, liquid bi-propellant rocket engine being developed to serve as an experim...
The development of liquid oxygen/liquid methane (LOX/LCH4) propulsion systems has recently become a ...
The Center for Space Exploration and Technology Research (cSETR) at The University of Texas at El Pa...
Amateur rocketry consists largely of rockets powered by solid propellant grains. The rocket industry...
Design and performance of liquid oxygen-liquid hydrogen thrust chamber for M-1 engin