Lessons learned during TBCC design for the NASA-AFRL joint system study /

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)

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

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

Advanced electric propulsion for RLV launched geosynchronous spacecraft /
by: Oleson, Steven R. (Steven Robert), 1964-
Published: (1999)

Two-stage reusable launch system utilizing a winged core vehicle and glideback boosters /
Published: (1989)

The effects of inlet turbulence and rotor/stator interactions on the aerodynamics and heat transfer of a large-scale rotating turbine model : IV--aerodynamic data tabulation /
by: Dring, Robert P.
Published: (1988)

The effects of inlet turbulence and rotor/stator interactions on the aerodynamics and heat transfer of a large-scale rotating turbine model : IV--aerodynamic data tabulation /
by: Dring, Robert P.
Published: (1988)

Reusable Reentry Satellite (RRS) summary report : propulsion system trade study.
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)

Payload performance analysis for a reusable two-stage-to-orbit vehicle /
by: Tartabini, Paul V.
Published: (2015)

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

Development of a high power microwave thruster, with a magnetic nozzle, for space applications /
by: Power, John L.
Published: (1989)

Development of a high power microwave thruster, with a magnetic nozzle, for space applications /
by: Power, John L.
Published: (1989)

Control activity in support of NASA Turbine Based Combined Cycle (TBCC) research /
Published: (2010)

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)

Flight motor set 360L001 (STS-26R). final report /
by: George, Russell J.
Published: (1989)

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

Emerging Communication Technologies (ECT) phase 3 final report /
Published: (2004)

Dynamic testing of the NASA Hypersonic Project combined cycle engine testbed for mode transition experiments /
Published: (2011)

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

Structural sizing of a 25 000-lb payload, air-breathing launch vehicle for single-state-to-orbit /
by: Roche, Joseph M., et al.
Published: (2001)

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

Testing of the NASA Hypersonics project's Combined Cycle Engine Large Scale Inlet Mode Transition Experiment (CCE LIMX) /
Published: (2012)

RL10 engine ability to transition from Atlas to Shuttle/Centaur program /
by: Baumeister, Joseph F.
Published: (2015)

CFD for hypersonic propulsion /
by: Povinelli, Louis A.
Published: (1991)

Fairing separation analysis using SepTOOL /
by: Zalewski, Bartlomiej Francisze, et al.
Published: (2015)

Hot gas ingestion test results of a two-poster vectored thrust concept with flow visualization in the NASA Lewis 9- x 15-foot low speed wind tunnel /
Published: (1990)

A performance comparison of two small rocket nozzles /
by: Arrington, Lynn A., et al.
Published: (1996)

RL10A-3-3A rocket engine modeling project /
by: Binder, Michael, et al.
Published: (1997)

Design and calibration of the X-33 flush airdata sensing (FADS) system /
by: Whitmore, Stephen A., et al.
Published: (1998)

Experiment module/support module interface specification for the reusable reentry satellite /
Published: (1991)

Proposed flight research of a dual-bell rocket nozzle using the NASA F-15 airplane /
by: Jones, Daniel S., et al.
Published: (2013)

Outline for reusable reentry satellite system specification : volumes 1 - volume 9 /
Published: (1989)

Hybrid propulsion technology program : final report.
Published: (1990)