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Lord, D. R.

Publications and source records attributed to Lord, D. R..

14 records
All sourcesNASA NTRSDOE OSTI
NASA NTRS1978

Spacelab development and its operational verification

This paper gives a brief status report on the current Spacelab program and describes how the results of ground and flight tests will be combined to provide the operational verification of the system. For the on-going project, data on design, testing and fabrication plans are presented. In particular, recent changes to meet the constraints of a 'build-to-cost' project are described. In the operational verification of Spacelab, ground and flight tests which ESA and NASA will perform are addressed. The installation of test instrumentation and the performance of integrated tests will be accomplished in the US. Experiments for the first flight will be integrated into Spacelab racks and pallets and simulated mission tests performed. On-orbit, system thermal surveys are planned and stress data will be obtained during launch and re-entry.

Bignier, M.↗
NASA NTRS1976

Spacelab - New tool for research and investigations in space

The Orbiter/Spacelab system is regarded as an entity that provides an orbital platform for experiments in a wide variety of scientific and technological fields. The paper presents a brief summary of the Spacelab system and its operation as an introduction to a new tool to be available to an international community of users through the 1980s. Investigations have shown that all the more conventional fields of space research and applications can benefit from the use of Spacelab, such as astronomy, magnetospheric physics, remote sensing, communications, and many others. It is expected that new areas that would gain from using Spacelab will be recognized as its operational life matures. Numerous sketches and photographs supplement the text.

Gibson, R.↗
NASA NTRS1976

Spacelab programme overview

The current activity status of Spacelab, objectives of which are to provide a laboratory and observation facility in space, is surveyed. Program requirements are given, and the basic Spacelab concept is described. The programmatic aspects of the program and some considerations concerning payload integration and payload operations are outlined.

Lord, D. R.↗
NASA NTRS1974

Spacelab status report

This paper describes the status of the Spacelab program to date, including the current baseline configuration and subsystems. Emphasis is placed on the features afforded to researchers and experimenters and approaches to experiment accommodation. The status of planning for use of the Spacelab is described as well as the role and training of the payload specialist. Several typical missions are presented to show how these concepts might be implemented. Discussion of the roles and responsibilities of the NASA and the European Space Agency in development of the Spacelab is included.

Lord, D. R.↗
NASA NTRS1973

The design and utilization of a spacelab for sortie missions

Consideration of the feasibility of a 'sortie' type mission in which a manned laboratory is carried into near-earth orbit for a 7- to 30-day mission and is then returned to earth for reconfiguration and subsequent reflight. The fundamental difference in approach between the proposed Spacelab and concepts previously considered for space stations is that the spacelab will remain attached to the Shuttle Orbiter during its entire mission in space. An important trend in the design approach is the introduction of structural modularity of the Spacelab. Another factor which has been a significant design consideration is the need to properly balance the Shuttle and Spacelab configuration over a wide range of aerodynamic regimes and landing conditions. Also considered are the requirements which may be placed on the laboratory by potential users in fields of science and space applications.

Lord, D. R.↗
NASA NTRS1973

The space station: Key to living in space

Design and scientific equipment for the Manned Orbiting Laboratory and Skylab are elaborated. Multideck designs accommodate both zero gravity and artificial gravity conditions as well as a core module potentially useful as a planetary mission module for a 12-man crew. Artificial gravity approaches consider assembly rotation and differential spin rates for the various decks. Counterrotation systems are projected to go from a station to a 50-man space base concept.

Lord, D. R.↗
NASA NTRS1970

An overview of NASA's Space Station program

NASA space station program, discussing relationship between space stations, Skylab and space shuttle, electric power generation, habitability, safety and communications networks

Lohman, R. L.↗
NASA NTRS1957

Tabulated Pressure Data for a Series of Controls on a 40 Deg Sweptback Wing at Mach Numbers of 1.61 and 2.01

An investigation has been made at Mach numbers of 1.61 and 2.01 and Reynolds numbers of 1.7 x l0(exp 6) and 3.6 x l0(exp 6) to determine the pressure distributions over a swept wing with a series of 14 control configurations. The wing had 40 deg of sweep of the quarter-chord line, an aspect ratio of 3.1, and a taper ratio of 0.4. Measurements were made at angles of attack from 0 deg to +/- 15 deg for control deflections from -60 deg to 60 deg. This report contains tabulated pressure data for the complete range of test conditions.

AERODYNAMICS↗