PERFORMANCE OF VARIABLE TWO-DIMENSIONAL INLET DESIGNED FOR ENGINE-INLET MATCHING. I - PERFORMANCE AT DESIGN MACH NUMBER OF 3.07
Supersonic performance of variable two-dimensional inlets designed for engine-inlet matching
ENGINE↗
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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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INVESTIGATION OF A 0.6 HUB-TIP RADIUS-RATIO TRANSONIC TURBINE DESIGNED FOR SECONDARY-FLOW STUDY. III - EXPERIMENTAL PERFORMANCE WITH TWO STATOR CONFIGURATIONS DESIGNED TO ELIMINATE BLADE WAKES AND SECONDARY-FLOW EFFECTS AND CONCLUSIONS FROM ENTIRE STATOR INVESTIGATION
Hub-tip radius ratio transonic turbine for secondary flow - stator configurations designed to eliminate blade wakes and secondary-flow effects
BOUNDARY LAYER↗
OFF-DESIGN AERODYNAMIC CHARACTERISTICS AT MACH NUMBERS 1.61 AND 2.20 OF A SERIES OF HIGHLY SWEPT ARROW WINGS DESIGNED FOR MACH NUMBER 2.0 EMPLOYING VARIOUS DEGREES OF TWIST AND CAMBER
Off-design aerodynamic characteristics of swept arrow wings with twist and camber at supersonic velocities
OCULOGYRAL ILLUSION↗
DESIGN CRITERIA FOR ZERO-LEAKAGE CONNECTORS FOR LAUNCH VEHICLES. VOLUME I, SUMMARY, CONCLUSIONS, AND DESIGN EXAMPLES
Design criteria for zero-leakage connectors for launch vehicles - plastic flow & flange rolling
LAUNCH VEHICLE↗
The role of spatial imigination in the work of the designer and in the teaching of drawing in technical schools the role of spatial imagination in the work of the designer and in the teaching of drawing in technical schools
Role of spatial imagination in designing and in teaching of drawing in technical schools
TRAINING↗
Power relay design. analyze, study and estab- lish an optimum power relay design for application in saturn launch vehicle systems summary report, jan. - jul. 1962
Contactor characteristics and power relay design for application in Saturn launch vehicle systems
CONTACT POTENTIAL↗
Voyager design studies. volume v- lander design, part ii
Engineering and design data for Voyager Mars and Venus lander systems
LANDING SYSTEM↗
Voyager design studies. volume v- lander design, part i
Engineering and conceptual design of landing system for Voyager unmanned spacecraft
UNMANNED SPACECRAFT↗
Surveyor lunar roving vehicle, phase I. Volume III - Preliminary design and system description. Book 2 - Validation of preliminary design Final report
Validation of preliminary design for Surveyor lunar roving vehicle - mobility, structure, deployment, folding and erection mechanism, and Apollo support scientific experiments
SURVEYOR PROJECT↗
Constricted high enthalpy arc heater design and performance data, including calculations for a 10 MW design First interim technical report
Performance prediction and design analysis of constricted coaxial-flow arc air heaters for materials testing and atmospheric entry simulation
ARC HEATING↗
Voyager spacecraft system. Preliminary design, volume A /book 2 of 4/ - Flight spacecraft preferred design - Telecommunications
Telecommunication system requirements and design for Voyager spacecraft 1971
VOYAGER PROJECT↗
Voyager spacecraft system. Preliminary design, volume A /book 4A of 4/ - Flight spacecraft preferred design - Implementation
Voyager project organization, management, scheduling and implementation of spacecraft design, and support scheduling
PROGRAM MANAGEMENT↗
Voyager spacecraft system. Preliminary design, volume B /book 2 of 3/ - Alternate designs considered - Telecommunications
Voyager spacecraft trade-off design parameters in telecommunication subsystems and between telecommunication system and other systems - data encoder and data storage systems
VOYAGER PROJECT↗
Voyager spacecraft system. Preliminary design, volume C - 1971 operational support equipment design
Operational support equipment design for Voyager spacecraft - system test and launch complex equipment
LAUNCH COMPLEX↗
Voyager spacecraft system - Preliminary design. 1969 test spacecraft design, volume D
Spacecraft functional description, mission objectives, design characteristics and system requirements of 1969 Voyager test flight
PROGRAM MANAGEMENT↗
Development of the Circuit Design from the Logic Design of a Random Walk Machine Final Report
Logic design of small, high speed, random walk machine for solving Laplace equation
LOGIC CIRCUIT↗
Preliminary design study of SLAMAST Scout- launched advanced materials and structures test-bed. Volume II - Design feasibility
Design feasibility of Scout launched recoverable lifting reentry vehicle test bed
REENTRY VEHICLE↗
Brayton-cycle radioisotope heat-source design study. Phase II /preliminary design/ report
Brayton cycle radioisotope heat source design
RADIOACTIVE ISOTOPE↗