Decomposing solid micropropulsion nozzle performance issues /

Flight motor set 360L002 (STS-27R). final report /
by: Meyer, S. A.
Published: (1989)

Converging-diverging nozzle thruster code for nuclear or chemical rocket performance computations /
by: Juhasz, Albert J.
Published: (2019)

Internal thrust and pumping performance of an auxiliary inlet ejector nozzle with clamshell thrust reverser /
by: Mansour, Ali H., et al.
Published: (1969)

A survey of challenges in aerodynamic exhaust nozzle technology for aerospace propulsion applications /
by: Shyne, Rickey J.
Published: (2002)

A survey of challenges in aerodynamic exhaust nozzle technology for aerospace propulsion applications /
by: Shyne, Rickey J.
Published: (2002)

Theoretical study on the effect of the design of small (milli-newton) thruster jets on molecular contamination for the space station /
by: Riley, Ben R.
Published: (1986)

Lessons learned during TBCC design for the NASA-AFRL joint system study /
by: Snyder, Christopher A., et al.
Published: (2013)

Investigation of low-Reynolds-number rocket nozzle design using PNS-based optimization procedure /
by: Hussaini, M. Moin, et al.
Published: (1996)

Effects of nozzle exit geometry and pressure ratio on plume shape for nozzles exhausting into quiescent air /
by: Scallion, W. I.
Published: (1991)

Analysis and design of optimized truncated scarfed nozzles subject to external flow effects /
by: Shyne, Rickey J.
Published: (1990)

Conceptual design for a dual-bell rocket nozzle system using a NASA F-15 airplane as the flight testbed /
by: Jones, Daniel S.
Published: (2014)

Aeropropulsive characteristics of isolated combined turbojet/ramjet nozzles at Mach numbers from 0 to 1.20 /
by: Carson, George T., et al.
Published: (1988)

Solid rocket booster thrust vector control subsystem description /
Published: (1983)

Advanced liquid rockets /
by: Schneider, Stephen J.
Published: (1992)

NEXT propellant management system integration with multiple ion thrusters /
by: Sovey, J. S.
Published: (2011)

Methodology for three dimensional nozzle design /
by: Ferri, Aldo A., et al.
Published: (1974)

Measured pressure distributions inside nonaxisymmetric nozzles with partially deployed thrust reversers /
by: Green, Robert S.
Published: (1987)

Measured pressure distributions inside nonaxisymmetric nozzles with partially deployed thrust reversers /
by: Green, Robert S.
Published: (1987)

Multidisciplinary approach to aerospike nozzle design /
by: Korte, J. J.
Published: (1997)

Exhaust nozzle plume effects on sonic boom test results for isolated nozzles /
by: Castner, Raymond S.
Published: (2011)

Integrity of the plasma magnetic nozzle /
by: Gerwin, Richard A.
Published: (2009)

Flow processes in overexpanded chemical rocket nozzles.
by: Schmucker, Robert H.
Published: (1984)

Static and dynamic deflection studies of the SRM aft case/nozzle joint /
by: Christian, David C.
Published: (1989)

Calibration for thrust and airflow measurements in the CE-22 Advanced Nozzle Test Facility /
by: Werner, Roger A.
Published: (2010)

Static internal performance of a single-engine nonaxisymmetric-nozzle vaned-thrust-reverser design with thrust modulation capabilities /
by: Leavitt, Laurence D.
Published: (1985)

Trade study of multiple thruster options for the Mars airplane concept /
Published: (2009)

Separate flow nozzle test status meeting : proceedings of a conference held at and sponsored by NASA Glenn Research Center, Cleveland, Ohio, September 9-10, 1997 /
Published: (2000)

RSRM-9 (360L009) final report : ballistics mass properties /
by: Drendel, Albert S.
Published: (1990)

Experimental evaluation of a translating nozzle sidewall radial turbine /
by: Roelke, Richard J.
Published: (1987)

Static performance of a fixed-geometry exhaust nozzle incorporating porous cavities for shock-boundary layer interaction control /
by: Asbury, Scott C., et al.
Published: (1999)

Derivation of the data reduction equations for the calibration of the six-component thrust stand in the CE-22 advanced nozzle test facility /
by: Wong, Kin C.
Published: (2003)

Robust exploration and commercial missions to the moon using nuclear thermal rocket propulsion and lunar liquid oxygen derived from FeO-rich pyroclastic deposits /
by: Borowski, Stanley K.
Published: (2018)

Experimental and analytical study of close-coupled ventral nozzles for ASTOVL aircraft /
by: McArdle, Jack G.
Published: (1990)

An experimental comparison of nonswirling and swirling flow in a circular-to-rectangular transition duct /
by: Reichert, Bruce A.
Published: (1991)

Flow processes in overexpanded chemical rocket nozzles.
by: Schmucker, Robert H.
Published: (1984)

Solid hydrogen experiments for atomic propellants : particle formation energy and imaging analyses /
by: Palaszewski, Bryan Alan Richard
Published: (2002)