Saturn monthly progress report, december 16, 1963 - january 16, 1964
Saturn I launch vehicle, Saturn IB launch vehicle, and Saturn V launch vehicle components and configuration
SATURN V LAUNCH VEHICLE↗
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Results for “SATURN IB LAUNCH VEHICLE”
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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Saturn monthly progress report, august 15 - september 18, 1963
Saturn I launch vehicle, Saturn IB launch vehicle, and Saturn V launch vehicle components and configuration
SATURN V LAUNCH VEHICLE↗
Minutes of the vehicle mechanical design integration working group meeting no. 6, s-ivb stage /saturn ib/v/
Mechanical design integration of Saturn S- IVB STAGE of Saturn IB and Saturn V launch vehicle configuration
LAUNCH VEHICLE CONFIGURATION↗
Test report for proportional controller /temperature/, Johnson Service Company part number T-900, NASA drawing number 75M04406 PPC-2
Inspection and testing of proportional temperature controller for air conditioning system of Saturn IB launch vehicle
SATURN IB LAUNCH VEHICLE↗
Techniques of implementing launch automation programs - Saturn IB space vehicle system.
Automated techniques for providing reliability assurance in launch operations of Saturn IB SPACE vehicle system
SPACE VEHICLE CHECKOUT PROGRAM↗
Man's transportation to space
Saturn i, saturn ib, and saturn v launch vehicles
SATURN IB LAUNCH VEHICLE↗
Saturn ib liquid hydrogen orbital experiment definition
Proposed liquid hydrogen orbital experiment using Saturn IB launch vehicle
SATURN IB LAUNCH VEHICLE↗
Compound pressure and vacuum relief valve, 2-inch. Ladewig Valve Company part number 3302- F, NASA drawing number 75 M04406 PRV-3
Functional and environmental testing of compound pressure and vacuum relief valve for Saturn Ib launch vehicle
FUNCTION TEST↗
Saturn ib mission plan and technical information check list, volume ii
Saturn IB launch vehicle configuration and test objectives and measuring program with technical check list covering Saturn S- IB stage and Saturn S- IVB stage
SATURN S-IVB STAGE↗
Transonic aerodynamic characteristics of a saturn ib-apollo launch vehicle with various upper-stage configurations
Transonic wind pressure tunnel investigation for aerodynamic characteristics of Saturn IB APOLLO launch vehicle with various upper stage configurations
SATURN IB LAUNCH VEHICLE↗
The aeroelastic characteristics of the Saturn-IB SA-201 launch vehicle
Aerodynamic damping determined as function of static load distribution for Saturn IB SA-201 VEHICLE from subsonic to supersonic speeds
SUPERSONIC SPEED↗
The aeroelastic characteristics of the Saturn IB SA-203 launch vehicle
Aeroelastic properties, and effects of boundary layer-terminal shock wave interaction on Saturn IB SA-203 launch vehicle
AEROELASTICITY↗
First Apollo Space Test Set for Feb. 23
Projected launch and operation of Apollo-Saturn space vehicle
SATURN IB LAUNCH VEHICLE↗
Techniques of Implementing Launch Automation Programs /saturn IB Space Vehicle System/
Launch automation programs for Saturn IB SYSTEM utilizing digital computer techniques to increase vehicle reliability from manufacturing through prelaunch checkout
CHECKOUT EQUIPMENT↗
Skylab status report.
The laboratory will be launched on Apr. 30, 1973, aboard a Saturn V vehicle. Approximately twenty-three and a half hours later the first crew will be launched in a command and service module aboard a Saturn IB launch vehicle. The laboratory will consist of modules. The orbital workshop (OWS) is made from the liquid oxygen and liquid hydrogen tanks of a Saturn S-IVB third stage. The OWS contains the living quarters and two experiments areas. The airlock sits on top of the OWS and contains the controls and hatch for the extra-vehicular activity.
Conrad, C., Jr.↗
Saturn ib mission plan and technical information checklist, volume ii
Saturn IB mission planning - testing, measuring, configuration and instruments for Saturn S- IB STAGE and Saturn S- IVB stage
MISSION PLANNING↗
The aeroelastic characteristics of the Saturn-IB and Saturn-V launch vehicles
Effects of flow separation on aeroelastic characteristics of Saturn IB and Saturn V launch vehicles with Apollo payload
FLOW SEPARATION↗
Advanced digital circuit R and D evaluation Final report, 3 Oct. 1964 - 30 Sep. 1965
Evaluation and testing of suitability of using integrated circuits in Saturn IB and launch vehicle data adapter
SATURN IB LAUNCH VEHICLE↗