Abstract: A flow regulator for high-pressure fluids at elevated temperatures includes a body having a flow passage extending between inlet and outlet openings. First and second orifice members are arranged in the flow passage so at least one of the orifice members can be moved transversely in relation to the flow passage between one operating position where the two orifice openings are aligned for establishing a maximum flow rate of fluids flowing through the flow passage and at least one other operating position in which the two openings are moderately misaligned with one another for establishing a predetermined reduced flow rate of fluids flowing through the flow passage.
Type:
Grant
Filed:
April 11, 1990
Date of Patent:
June 4, 1991
Assignee:
The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
Abstract: A process for manufacturing a low density ceramic powder which can be formed to make a lightweight material for insulation or other construction. The ceramic product made from the process has a final density of less than 25% to about 1% of its theoretical weight of the ceramic powder. The ceramic product is lightweight and can be made to withstand high temperatures greater than 1400.degree. C.
Type:
Grant
Filed:
June 30, 1988
Date of Patent:
April 24, 1990
Assignee:
The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
Abstract: A triangular space station deployable in orbit. The framework is comprised of three trusses, formed of a pair of generally planar faces comprised of foldable struts which expand and lock into rigid structural engagement forming a repetition of equilateral triangles and non-folding diagonal struts interconnecting the two faces. The struts are joined together by node fittings. The framework can be packaged into a size and configuration which can be transported by a space shuttle orbiter in a single orbital flight and when deployed, provides large work/construction area and ample planar surface area for solar panels and thermal radiators. A plurality of modules are secured to the framework and then joined by tunnels to comprise an interconnected modular array disposed along the free edges of the framework. Thruster units for space station orientation and altitude maintenance are provided.
Type:
Grant
Filed:
March 9, 1984
Date of Patent:
April 1, 1986
Assignee:
The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
Inventors:
William C. Schneider, Reginald B. Berka, Herbert C. Kavanaugh, Kornel Nagy, Richard C. Parish, John A. Schliesing, Paul D. Smith, Frederick J. Stebbins, Clarence J. Wesselski