Subliming solid control rocket, phase I Final report
Subliming solid propellant attitude control rocket
SEARCH · Engineering Papers
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.
Quote a phrase for an exact phrase match. Source license links do not imply unrestricted reuse.
Subliming solid propellant attitude control rocket
Vibration effects on mass and convective heat transfer under vacuum sublimation conditions
Heat and mass transfer rate dependence on vibration velocity of body undergoing vacuum sublimation with steady state free convection conditions
Comparison of chlorine or iodine use as feedwater bactericides in lunar excursion module cooling system sublimator
Ultrahigh vacuum produced by combination of turbomolecular and titanium sublimation pumping
This project, sponsored by the NASA Innovative Advanced Concepts examines how the systematic use of space resources such as frozen volatiles can create a new paradigm in surface power generation for deep space missions. The ubiquitous presence of ices of water, carbon dioxide and other compounds throughout the Solar System under conditions favorable for their sublimation will enable novel in-space propulsion and actuation concepts to become a reality and to address one of NASA's Grand Challenges of "All Access Mobility." Accessing such a resource in the far corners of our interplanetary neighborhood let us conceive exploration missions capable of refueling in the Jovian and Saturnian systems to achieve new goals or reach new destinations. The concept also has potential to apply in-situ propulsion to a comet or an asteroid to deflectits orbit slightly to avoid a future encounter with Earth.
Free flight investigations with solid fuel rocket propelled vehicle systems where the thermal protection was provided by either a subliming ablator or by transpiration cooling
Free flight tests of subliming ablators and transpiration cooling as thermal protection at hypersonic speeds
Radioisotopic continuous measurement techniques for determination of heat shield ablation and sublimation
Heat-shield sublimation and ablation determination during atmospheric reentry, using radioactive technique
Sublimated titanium as a gettering agent in conjunction with a turbine-type pump provides a two-step procedure for obtaining an ultrahigh vacuum of 10 to the minus 11 torr. The pump alone evacuates the chamber to a pressure of 10 to the minus 9 torr. The residual gas is removed by the gettering agent at a pumping speed of 15 liters per second per square inch.
Volcanic sublimates and secondary impact craters of Liamana Volcano, Hawaii, with reference to lunar craters
Two subliming solid propellant thrustor systems for spacecraft attitude control
Flight subliming solid respin rocket system development for OV2-1 satellite and nozzle optimization performance studies
Thermal energy supply improvements to uprate performance of subliming solid control rocket
Knudsen measurements of sublimation of manganese selenide based on vaporization reaction with variable temperature and pressure
MnSe sublimation Knudsen measurements at various temperatures and pressures noting congruent vaporization
Subliming solid reaction control system design, operation and test for ATS