High temperature stable carborane adhesives Second quarterly progress report, Mar. 21 - Jun. 20, 1966
Polymerization and synthesis of carborane-epoxy adhesives for high temperature aerospace technology
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Polymerization and synthesis of carborane-epoxy adhesives for high temperature aerospace technology
Thermal stability of double zirconium silicate pigment coatings, and of potassium silicate treated zinc oxide and silicone paints
Synthesis of 1-methyl-3, 5-diphenylthiabenzene 1-oxide suggests possibility of ylide-like character although ylene-like is not discounted
Buoyancy and magnetohydrostatic stability of magnetic body immersed in magnetizable fluid
Space simulation tests on temperature control, inorganic and silicone coatings, zinc titanate pigment synthesis and evaluation, and silicone photolysis
Thin film convective heat transfer gage functions effectively for prolonged periods at temperatures up to 1000 degrees F. An initial resistance shift does not inhibit the performance or accuracy of the gages, as the original resistance-temperature relationship remains unchanged.
Poppet-type check valve design accommodates a wide flow range without the usual chatter problem at low flow conditions. This pressure isolation check valve is proposed for the J-2 rocket pneumatic package.
Comparison is made of the power consumed and the acoustic amplification realized when a dc bias field is placed across a piezoelectric semiconductor and adjusted to amplify a microwave acoustic signal to the point where the forward gain is just equal to the reverse attenuation. This represents the maximum possible gain condition.
Synthesis of carborane-epoxy adhesives for high temperature aerospace applications
Explicit numerical methods for integrating coupled nonlinear ordinary differential equations with parasitic eignevalues
Numerical methods for integrating nonlinear differential equations with parasitic eigenvalues
Electromagnetic switching properties of bistable, magnetically permeable liquid bead with nondestructive memory for gas flow control
Soft landing spacecraft landing gear design for legged assemblies, discussing load, clearance and stability requirements
Reactive encapsulation methods for thermal stabilization of zinc orthotitanate resin paints for spacecrafts materials
Preparation of zinc oxide pigmented methyl silicone coating for thermal protection of space flight structures
Synthesis of Pyrrone laminates from sulfone dianhydride
Amplifier and stretcher system, which minimizes thermal effects and compensates for repetition-rate effects, maintains resolution levels in spectrum analysis. An additional inverting amplifier is used in the system to provide a noiseless charge restorer.
Control of vapor phase reaction kinetics to produce pigments by homogeneous nucleation