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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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At least 1,135 records · Page 63

All sources NASA NTRS DOE OSTI

NASA NTRS1978

Update on the development of the Space Shuttle main engine /as of June 20, 1978/

During the last year, significant progress was made toward the development of the Space Shuttle Main Engine which will provide propulsion for the Space Shuttle Orbiter Vehicle. Component and subsystem testing was conducted at the Rocketdyne Santa Susana Field Laboratory on combustion devices, turbomachinery, and the engine POGO suppression system. Engine testing continued at the National Space Technology Laboratories on both single engines and a three-engine cluster. As a result of these tests, hardware limitations were identified and design modifications were incorporated and evaluated by further testing. Current effort is being directed toward the delivery of the first flight engines and certification of the SSME for manned flight.

Johnson, J. R.↗

NASA NTRS1979

Performance verification of an air solar collector

Procedures and results of battery of qualification tests performed by independent certification agency on commercial solar collector are presented in report. Reported results were used as basis in judging collector suitable for field installation in residential and commerical buildings.

Miller, D. C.↗

NASA NTRS1979

Development of nonmetallic solar collector and solar-powered pump

Design and building of two unique components for solar heating (1. flatplate solar collector using no metal components, and 2. solar powered pump for heating and cooling systems are outlined in report. Report also discusses hardware, deliverable end items, problems encountered during fabrication and testing, and performance certification.

Parker, J. C.↗

NASA NTRS1980

Final report on the concentric-tube solar collector

Report documents 26-month program to optimize performance of commercial high performance concentric tube solar collector. Report discusses program objectives, accomplishments, encountered problems, and final hardware. Certification test results are also included.

Parker, J. C.↗

NASA NTRS1980

Concentrating solar collector - final design

Final report of program to improve commercially available concentrating solar collector describes final hardware, discusses problems encountered, and presents certification statements, photographs, and recommendations for modification.

Parker, J. C.↗

NASA NTRS1978

Trends in Langley helicopter noise research

A broad perspective of needs in helicopter exterior and interior control is presented. Emphasis is given to those items which support noise certification of civil helicopters and which result in reduced environmental noise impact to community residents as well as to helicopter passengers. The activities described are related to the Langley responsibilities for helicopter acoustics as defined by NASA roles and missions.

Hubbard, H. H.↗

NASA NTRS1979

Aircraft icing: Introduction

The objectives of the Workshop were as follows: (1) to assess the current understanding of fixed wing and rotorcraft operational icing environments and problems (2) to evaluate facilities requirements for R&D and certification purposes (3) to examine means of improving icing forecasts (4) to identify shortcomings in aeronautical icing knowledge which can be alleviated by new research and instrumentation development.

Enders, J. H.↗

NASA NTRS1979

A review of the icing situation from the standpoint of general aviation

An overview of the present situation in the field of aircraft icing with respect to certification and operation of nontransport category airplanes is given. Problems of definition and inconsistencies are pointed out. Problems in the forecasting and measurement of icing intensities are discussed. The present regulatory environment is examined with respect to its applicability and appropriateness to nontransport airplanes.

Newton, D. W.↗

NASA NTRS1979

Quiet propulsive lift for commuter airlines

The performance of STOL or RTOL aircraft and NASA's research program to provide options for future design and certification of quiet propulsive-life transports is described.

Wilcox, D. E.↗

NASA NTRS1977

Shuttle communication systems compatibility and performance testing

The Shuttle communications system consists of major space and ground elements. The compatibility and performance of each of these major elements functioning as a complete system must be certified prior to operational missions. This paper discusses the Shuttle communication systems compatibility and performance testing. The system test philosophy for the complex communication channels is described in terms of the major phases, which include early breadboard system design evaluation tests, system development tests with prototype hardware, and system certification testing with qualifiable (flight) hardware. The system hardware configuration, facility requirements, test and evaluation techniques, and operational approaches required to accomplish each major phase of testing are reviewed. Results of recently completed space-to-space and space-to-ground system tests are presented. Test techniques and measurement accuracies proven over ten years of unique system-evaluation experience are reviewed. Techniques used in relating experimental and predicted system performance, and conclusions regarding the effectiveness of system level testing of such complex hardware, are addressed.

Seyl, J. W.↗

NASA NTRS1979

Optical system of the visual imaging subsystem on the Viking Orbiter spacecraft

The development of the optical system for the Viking Orbiter spacecraft is presented. Each spacecraft consisted of an orbiter and a lander, and the orbiter provided support during the lander descent, landing and operation on the Martian surface, and prior to separation the orbiter provided science data for site selection and certification. To support these objectives each orbiter carried twin camera systems with identical 475 mm f/3.5 telescopes. The development of the Visual Imaging Subsystem which used all spherical catadioptric cassegrains with all elements fabricated from pure fused silica and Mangin primary mirrors is described. Computer aided design optimization and the ray aberration analysis of the final design are presented. The Viking telescopes had high theoretical and measured performance and obtained many high quality images of the Martian surface.

Larks, L.↗

NASA NTRS1979

Development of the Space Shuttle Main Engine /May 1979/

During the last year, significant progress was made toward the development of the Space Shuttle Main Engine, which will provide propulsion for the Space Shuttle Orbiter vehicle. Engine system testing continued at the National Space Technology Laboratories on both single engines and a three-engine cluster. A third single engine test position was activated at the Rocketdyne Santa Susana Field Laboratory to provide additional capability for demonstrating increasing engine maturity and for solving problems. The results of engine system testing is discussed as well as the major problems identified and the design changes incorporated to solve those problems. A review of the program efforts toward the delivery of the first set of flight engines and the certification of the SSME for manned flight is included.

Colbo, H. I.↗

NASA NTRS1979

A graph-theoretic method to quantify the airline route authority

The paper introduces a graph-theoretic method to quantify the legal statements in route certificate which specifies the airline routing restrictions. All the authorized nonstop and multistop routes, including the shortest time routes, can be obtained, and the method suggests profitable route structure alternatives to airline analysts. This method to quantify the C.A.B. route authority was programmed in a software package, Route Improvement Synthesis and Evaluation, and demonstrated in a case study with a commercial airline. The study showed the utility of this technique in suggesting route alternatives and the possibility of improvements in the U.S. route system.

Chan, Y.↗

NASA NTRS1980

Thermosyphon heat exchanger

Report summarizes final development, testing, and certification of pumpless, liquid-to-air heat exchanger for solar heating. System requires blower but no pump in water loop. Output is 35,000 Btu/hr when water temperature is 49 C.

Hankins, J. D.↗

NASA NTRS1980

Controller and temperature monitor for solar heating

Report describes development and certification of 77-171 differential thermostat for controlling solar-heating and cooling systems and 77-180 temperature monitor of indoor, outdoor, and storage temperatures. Units are commercially available.

Hankins, J. D.↗

NASA NTRS1980

A summary of joint US-Canadian augmentor wing powered-lift STOL research programs at the Ames Research Center, NASA, 1975-1980

Several different flight research programs carried out by NASA and the Canadian Government using the Augmentor Wing Jet STOL Research Aircraft to investigate the design, operational, and systems requirements for powered-lift STOL aircraft are summarized. Some of these programs considered handling qualities and certification criteria for this class of aircraft, and addressed pilot control techniques, control system design, and improved cockpit displays for the powered-lift STOL approach configuration. Other programs involved exploiting the potential of STOL aircraft for constrained terminal-area approaches within the context of present or future air traffic control environments. Both manual and automatic flight control investigations are discussed, and an extensive bibliography of the flight programs is included.

Hindson, W. S.↗

NASA NTRS1980

Predicted airframe noise levels

Calculated values of airframe noise levels corresponding to FAA noise certification conditions for six aircraft are presented. The aircraft are: DC-9-30; Boeing 727-200; A300-B2 Airbus; Lockheed L-1011; DC-10-10; and Boeing 747-200B. The prediction methodology employed is described and discussed.

Raney, J. P.↗

NASA NTRS1979

Shuttle integration status

The paper examines systems certification methodology for the Space Shuttle. Attention is then given to recent activities that will enhance the capability of the Shuttle during the operational period; structural dynamics, main propulsion, and thrust augmentation are considered.

Morris, O. G.↗