Study of a contractors capabilities center and the technology transfer process Final report, 15 Mar. 1966 - 30 Jun. 1968
Feasibility of NASA Contractors Capabilities Center, and approaches to technology utilization
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.
Feasibility of NASA Contractors Capabilities Center, and approaches to technology utilization
Gas bearing gyroscope possessing high G and sterilization capability, utilizing low power spinmotor and high frequency pump
Rendezvous and station keeping simulator with fly around capability and virtual image vewing
Astronaut capability to maintain life support systems and cabin habitability in weightlessness
Aerodynamic characteristics of large-angle cones in supersonic lifting capabilities
Microwave radiometric sensor operational principles and capabilities, discussing antennas and radiometric receivers
Saturn 5 translunar payload capability encancement by fuel biasing, propellant utilization systems, trajectory shaping and programmed mixture ratio scheme
Self-checking technique detects defective solid state modules used in electronic test and checkout instrumentation. A ten bit register provides failure monitor and indication for 1023 comparator circuits, and the automatic fault-isolation capability permits the electronic subsystems to be repaired by replacing the defective module.
Universal sized vest, with specially tailored pockets designed to hold medical supplies, provides first aid/first care medical teams with broadened on-site capability. Vest is made of nylon, tough fibrous materials, and polyvinyl chloride. Design facilitates rapid donning, doffing, and adjustment.
Performance capability and vehicle dynamics of Saturn 5 launch vehicle for two engine out malfunctions for Saturn S-1C stage
Module 2 S-4B stage auxiliary propulsion system 90-day recycle capability test
Lunar module redesignation footprint capability during final approach
S-4b-5 auxiliary propulsion system 90-day recycle capability test
Analysis of capabilities and limitations of film air cooling methods for turbine engines
Solar electric propulsion /SEP/ for automated planetary missions, discussing system characteristics, capabilities and costs
Earth resources satellites capabilities and requirements emphasizing orbit parameters, remote sensing, data handling and telemetry systems
Apollo/Saturn 5 Kennedy Launch Complex 39 /LC-39/ physical characteristics emphasizing high launch rate capability, economy of operation and superior flexibility