Publication | Open Access
Mastering Cryogenic Propellants
32
Citations
35
References
2012
Year
Space VehicleEngineeringSpace VehiclesNumerical SimulationSpace Flight SystemsSpace SciencesThermodynamicsSpace Systems DesignSpacecraft MaterialsCryogenic Propellant DepotsCryogenic PropellantsRocket EnginePropulsionAerospace Propulsion SystemsHeat TransferSpacecraft EngineeringPropellant SloshAerospace EngineeringCryogenicsIn-space Propulsion SystemsAerospace PropulsionCold Gas PropulsionSpace Engineering
NASA Glenn Research Center began experimenting with cryogenic propellants in the early 1950s to explore high‑performance fuels for liquid rocket engines, and later recognized their essential role for space missions, prompting agency focus. The goal was to support the development of the Centaur upper stage and Saturn S‑IVB stage by initiating extensive technology development for in‑space cryogenic fluid management (CFM). Researchers learned to design cryogenic systems and develop safe procedures, addressing propellant slosh, settling, and short‑term storage/pressure control to enable reliable in‑space CFM. Early work established a core skill set, and over the years NASA GRC advanced CFM technologies, now poised to enable long‑duration in‑space cryogenic propulsion stages and depots.
The National Aeronautics and Space Administration (NASA) Glenn Research Center (GRC) began experimentation with cryogenic propellants in the early 1950s to understand the potential of these high-performance propellants for use in liquid propellant rocket engines. Supporting these tests required learning how to both design cryogenic systems and develop procedures to safely and reliably work with cryogenic fuels and oxidizers. This early work led to the development of a skill set that has been core to the center ever since. When NASA was formed and the exploration missions were defined, it became clear that the ability to use cryogenic propellants in the thermal and microgravity environment of space was critical to mission success, and the agency was tasked with enabling this capability. To support development of the Centaur upper stage and the Saturn S-IVB stage, GRC researchers and engineers initiated extensive technology development for the in-space application of cryogenic fluid management (CFM). These initial efforts addressed basic requirements of propellant slosh, settling, and short-term storage/pressure control. Over the ensuing years, the NASA GRC has advanced CFM technologies to enable more reliable and capable upper stages. Today, these CFM technologies are on the brink of enabling long-duration in-space cryogenic propulsion stages and cryogenic propellant depots.
| Year | Citations | |
|---|---|---|
Page 1
Page 1