Experimental investigation of augmented spark ignition of a LO₂/LCH₄ reaction control engine at altitude conditions /

Mars Spark Source Prototype /
by: Eichenberg, Dennis J.
Published: (1999)

Experimental evaluation of the ignition process of carbon monoxide and oxygen in a rocket engine /
by: Linne, Diane L.
Published: (1996)

Correlation of helium solubility in liquid nitrogen /
by: Van Dresar, Neil T., et al.
Published: (2012)

Guide for oxygen hazards analyses on components and systems /
by: Stoltzfus, Joel M., et al.
Published: (1996)

NESC review of the 8-Foot High Temperature Tunnel (HTT) oxygen storage pressure vessel inspection requirements /
Published: (2009)

A heat transfer investigation of liquid and two-phase methane /
by: Van Noord, Jonathan
Published: (2010)

Altitude deviations : breakdowns of an error-tolerant system /
by: Palmer, Everett A.
Published: (1993)

Liquid methane conditioning capabilities developed at the NASA Glenn Research Center's Small Multi-purpose Research Facility (SMiRF) for accelerated lunar surface storage thermal testing /
Published: (2011)

Spontaneous ignition delay characteristics of hydrocarbon fuel-air mixtures /
by: Lefebvre, Arthur H. (Arthur Henry), 1923-2003
Published: (1986)

Breakdown characteristics of an isolated conducting object in a uniform electric field /
by: Grothaus, M. G.
Published: (1987)

Combustion characteristics in the transition region of liquid fuel sprays : final report, January 1983 - September 1985 /
by: Cernansky, N. P.
Published: (1986)

The revamping of an ignition test facility /
by: Kearns, Kimberly A.
Published: (2002)

Ignition and combustion characteristics of metallized propellants : semi-annual report (January 1990-June 1990) /
by: Turns, Stephen R.
Published: (1990)

The reduction of lunar regolith by carbothermal processing using methane /
by: Balasubramaniam, R.
Published: (2010)

Development of a closed-loop strap down attitude system for an ultrahigh altitude flight experiment /
by: Whitmore, Stephen A., et al.
Published: (1997)

Liquid oxygen thermodynamic vent system testing with helium pressurization /
by: Van Dresar, Neil T.
Published: (2014)

A densified liquid methane delivery system for the Altair ascent stage /
Published: (2010)

Design and analysis of an isokinetic sampling probe for submicron particle measurements at high altitude /
by: Heath, Christopher M.
Published: (2012)

Performance of the spacecraft propulsion research facility during altitude firing tests of the Delta III upper stage /
by: Meyer, Michael L.
Published: (1998)

Ignition of cellulosic paper at low radiant fluxes /
by: White, K. Alan
Published: (1996)

Atomization and mixing study : interim report /
by: Ferrenberg, A.
Published: (1983)

Identifiability of additive, time-varying actuator and sensor faults by state augmentation /
by: Upchurch, Jason M., et al.
Published: (2014)

Possible mechanisms for turbofan engine ice crystal icing at high altitude /
by: Tsao, Jen-Ching, et al.
Published: (2016)

The structure of dilute combusting sprays /
by: Shuen, J.-S
Published: (1985)

Pressure-volume-temperature (PVT) gauging of an isothermal cryogenic propellant tank pressurized with gaseous helium /
by: Van Dresar, Neil T., et al.
Published: (2014)

Navigation study for low-altitude Earth satellites /
by: Pastor, P. R.
Published: (1985)

Orbital transfer vehicle oxygen turbopump technology. final report /
Published: (1990)

NASA/USRA high altitude reconnaissance aircraft.
Published: (1990)

Approximate pressure distribution in an accelerating launch-vehicle fuel tank /
by: Nemeth, Michael P.
Published: (2010)

Damage tolerance analysis of a pressurized liquid oxygen tank /
Published: (2006)

Avionics and power management for low-cost high-altitude balloon science platforms /
by: Chin, Jeffrey, et al.
Published: (2016)

Helicopter acoustic flight test with altitude variation and maneuvers /
by: Watts, Michael E.
Published: (2016)

Preparation for scaling studies of ice-crystal icing at the NRC Research Altitude Test Facility /
by: Struk, Peter M.
Published: (2013)

Application of background oriented Schlieren for altitude testing of rocket engines /
by: Wernet, Mark P., et al.
Published: (2017)

Liquid oxygen propellant densification production and performance test results with a large-scale flight-weight propellant tank for the X33 RLV /
by: Tomsik, Thomas M.
Published: (2010)

Thrust augmentation measurements using a pulse detonation engine ejector /
by: Santoro, Robert J.
Published: (2003)