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Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.

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At least 397 records · Page 22
All sourcesNASA NTRSDOE OSTI
NASA NTRS2022

Will scavenging liquid oxygen from the propellant of lunar landers reduce net delivered mass?

Baseline oxygen (O2) needs for astronauts on lunar surface missions are satisfied through delivery in logistics landers. Supplying O2 through resources already present on the lunar surface could reduce the logistics load mass as well as the cost. The propellant tanks on the landers are the most abundantly accessible source for supplying the needed O2 to the crew. Calculations and analysis were performed on both 28-day missions and year-long missions to determine the amount of O2 able to be scavenged from propellant.

Angelina Rossini↗
NASA NTRSDate not supplied

Mini-Nozzles for Individual Fuel Elements for NTP Systems NETS

The Testing Reference Design (TRD) reactor and engine for Nuclear Thermal Propulsion (NTP) systems typically use a large single nozzle with regenerative cooling which contributes a significant portion of the engine mass. Furthermore, if a fuel element is damaged or the flow is otherwise compromised, stagnant or backflow is expected which would further damage the reactor and engine. Therefore, the current analysis attempts to solve this potential issue by considering individual, smaller nozzles allocated for each individual fuel element while also neglecting regenerative cooling flow due to lower hoop stresses from the chamber pressure. However, a material that can withstand the chamber temperatures should be considered such as molybdenum or tungsten or a mixture of the two.

Daria Nikitaeva↗