1-24 of 30 Books
A two-stage-to-orbit spaceplane concept with growth potential
A two-stage-to-orbit spaceplane concept with growth potential
By Unmeel B. Mehta
Subsonic-to-hypersonic aerodynamic characteristics for a winged, circular-body, single-stage-to-orbit spacecraft configuration
Subsonic-to-hypersonic aerodynamic characteristics for a winged, circular-body, single-stage-to-orbit spacecraft configuration
By W. Pelham Phillips
Analysis of a new rocket-based combined-cycle engine concept at low speed
Analysis of a new rocket-based combined-cycle engine concept at low speed
By S. Yungster
Advanced low-cost O₂/H₂ engines for the SSTO application
Advanced low-cost O₂/H₂ engines for the SSTO application
By B. David Goracke
Near-optimal operation of dual-fuel launch vehicles
Near-optimal operation of dual-fuel launch vehicles
By M. Ardema
Single-stage-to-orbit
Single-stage-to-orbit
By Delma C. Freeman
Advances in hypersonic vehicle synthesis with application to studies of advanced thermal protection systems
Advances in hypersonic vehicle synthesis with application to studies of advanced thermal protection systems
By Mark D. Ardema
Preliminary sizing of vertical take-off rocket-based combined-cycle powered launch vehicles
Preliminary sizing of vertical take-off rocket-based combined-cycle powered launch vehicles
By Joseph M. Roche
Preliminary assessment of using gelled and hybrid propellant propulsion for VTOL/SSTO launch systems
Preliminary assessment of using gelled and hybrid propellant propulsion for VTOL/SSTO launch systems
By Dennis G. Pelaccio
Human lunar mission capabilities using SSTO, ISRU, and LOX-augmented NTR technologies
Human lunar mission capabilities using SSTO, ISRU, and LOX-augmented NTR technologies
By Stanley K. Borowski
The Reusable Launch Vehicle Technology Program and the X-33 advanced technology demonstrator
The Reusable Launch Vehicle Technology Program and the X-33 advanced technology demonstrator
By Stephen A. Cook
Airbreathing/rocket single-stage-to-orbit design matrix
Airbreathing/rocket single-stage-to-orbit design matrix
By James L. Hunt
The control system for the X-33 linear aerospike engine
The control system for the X-33 linear aerospike engine
By Jerry E. Jackson
1994 NASA/USRA/ADP design projects
1994 NASA/USRA/ADP design projects
By Thomas Cruse
Transonic aerodynamic characteristics of a proposed wing-body reusable launch vehicle concept
Transonic aerodynamic characteristics of a proposed wing-body reusable launch vehicle concept
By A. M. Springer
A guidance and control assessment of three vertical landing options for RLV
A guidance and control assessment of three vertical landing options for RLV
By M. Gallaher
A collection of technical papers
A collection of technical papers
By Space Logistics Symposium (6th 1995 Houston, Tex.)
Reusable Launch Vehicle Technology Program
Reusable Launch Vehicle Technology Program
By Delma C. Freeman
Computational study of a McDonnell Douglas single-stage-to-orbit vehicle concept for aerodynamic analysis
Computational study of a McDonnell Douglas single-stage-to-orbit vehicle concept for aerodynamic analysis
By Ramadas K. Prabhu
Trade study plan for reusable hydrogen composite tank system (RHCTS)
Trade study plan for reusable hydrogen composite tank system (RHCTS)
By H. S. Greenberg
Test plans, lightweight durable TPS tasks, 1,2,4,5, and 6
Test plans, lightweight durable TPS tasks, 1,2,4,5, and 6
By H. S. Greenberg
Test plans, GCPS task 4, subtask 4.2, thrust structure development
Test plans, GCPS task 4, subtask 4.2, thrust structure development
By H. S. Greenberg
Damage tolerance of candidate thermoset composites for use on single stage to orbit vehicles
Damage tolerance of candidate thermoset composites for use on single stage to orbit vehicles
By Alan T. Nettles