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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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3 records
All sourcesNASA NTRSDOE OSTI
NASA NTRS1950

Starting of rocket engine at conditions of simulated altitude using crude monoethylaniline and other fuels with mixed acid

Experiments were conducted at sea level and pressure altitude of about 55,000 feet at various temperatures to determine starting characteristics of a commercial rocket engine using crude monoethylaniline and other fuels with mixed acid. With crude monoethylaniline, ignition difficulties were encountered at temperatures below about 20 degrees F. With mixed butyl mercaptans, water-white turpentine, and x-pinene, no starting difficulties were experienced at temperatures as low as minus 74 degrees F. Turpentine and x-pinene, however, sometimes left deposits on the injector face. With blends containing furfuryl alcohol and with other blends, difficulties were experienced either from appreciable deposits or from starting.

COMBUSTION - ROCKET ENGINES↗
NASA NTRS1952

Ignition Delay Experiments with Small-scale Rocket Engine at Simulated Altitude Conditions Using Various Fuels with Nitric Acid Oxidants / Dezso J. Ladanyi

Ignition delay determinations of several fuels with nitric oxidants were made at simulated altitude conditions utilizing a small-scale rocket engine of approximately 50 pounds thrust. Included in the fuels were aniline, hydrazine hydrate, furfuryl alcohol, furfuryl mercaptan, turpentine, and mixtures of triethylamine with mixed xylidines and diallyaniline. Red fuming, white fuming, and anhydrous nitric acids were used with and without additives. A diallylaniline - triethylamine mixture and a red fuming nitric acid analyzing 3.5 percent water and 16 percent NO2 by weight was found to have a wide temperature-pressure ignition range, yielding average delays from 13 milliseconds at 110 degrees F to 55 milliseconds at -95 degrees F regardless of the initial ambient pressure that ranged from sea-level pressure altitude of 94,000 feet.

XYLIDINE↗
DOE OSTI2025

CRADA Number NFE-22-09315 with Captis Aire LLC (CRADA Final Report)

Our goal is to provide an economically and environmentally advantageous capture technology to clean the air at industrial manufacturing facilities, especially wood products manufacturing facilities. There are hundreds of wood products manufacturing sites at which this capture technology could be implemented and thousands more sites in the broader 104 industries subject to the clean air act. This work is critical because when implemented at just 50 wood products sites it could capture over 100 million pounds per year of pollutants (wastes) that could be converted into over 90 million pounds per year of valuable products rather than burning them as waste. These pollutants, primarily turpentine or terpenes, can be used to provide a wide variety of products including biofuels, flavors, fragrances, and more. Versus the baseline technology, the technology could reduce energy use including fossil fuels by more than 10 trillion BTUs per year and drive down operational costs for our customers by up to $150 million per year.

54 ENVIRONMENTAL SCIENCES↗