The saturn v fueldraulic gimbal system.
Kerosene as hydraulic fluid in gimbal actuation system of saturn v booster
SEARCH · Engineering Papers
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.
Quote a phrase for an exact phrase match. Source license links do not imply unrestricted reuse.
Kerosene as hydraulic fluid in gimbal actuation system of saturn v booster
Hydrostatic pressurized gas lubricated journal and thrust bearings for gyroscope gimbal bearings - static and dynamic load and flow analysis
Dynamic stability of free-free circular cylindrical shell subjected to gimballed variable end thrust
Phenol resin bonded, woven glass and Teflon fiber lubricant for J-2 rocket engine gimbal system
Static and dynamic characteristics of Centaur gimbal system under thrust loading
Bellows restraints, thrust-vector attitude-control gimbal devices, and tube clamp descriptions
Liquid propellant feed ducting and engine gimbal lines for Saturn vehicles
Reliability analysis of Centaur inertial guidance system first gimbal stabilization loop
Superconducting gyroscope for gimballed platform application
A two axis optical gimbal mechanism for aligning 1 meter diameter telescope primaries and test flat mirrors at temperatures from 300 to 4.2 K is being constructed for use in the Cryogenic Telescope Test Facility.
Tonopah Test Range (TTR), in support of its testing mission and modernization effort acquired a fleet of new gimballed tracking mounts (GTMs) manufactured by BAE Systems. The new GTMs can be operated remotely during flight tests and provide near real-time target tracking data. Furthermore, test vehicle Time-Space-Position-Information (TSPI) is evaluated using post-test synchronized imagery and pointing angle measurements acquired from each tracking mount. To comply with the Nuclear Enterprise Assurance Program (NEAP), all measurements devices must be certified. In keeping with the NEAP program, qualification of the new GTMs have been assessed to confirm that their pointing angle measurements produce acceptable TSPI results. This study only evaluated the four GTMs as a stand-alone solution and found that the GTMs meet their performance requirement of 0.006 degrees RMS error (or less) for post-processed pointing angles and produced TSPI solution with error volumes on the order of one meter or less. The new GTMs will be utilized in combination with existing optical tracking mounts, which will only improve the accuracy of the resulting TSPI data product. Details regarding the approach, analysis, summary results, and conclusions are presented.
Ball-and-socket joints are used to connect two rotating inputs to orthogonally pivoted outputs. This provides an accurate biaxial gimbal which will operate in continuous motion without backlash.
Saturn V S-IC stage engine guidance, flight control and gimbal servoactuation system for Apollo spacecraft
Damping and mass stiffness discontinuity effects on dynamic stability of free-free beam under gimballed pulsating end thrust
Satellite attitude stabilization using gimballed star trackers, analyzing satellite and star tracker motion in terms of angular velocity
Pneumatic gimbal actuator
Operational performance tests on dry lubricated ball bearings under simulated gimbal oscillation in vacuum
Mathematical model and computer program for analysis of three and four gimbal systems