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NASA NTRS · 19940018584

Dual-bell altitude compensating nozzles

Abstract

The primary objective of this cold flow test effort was to assess the performance characteristics of dual bell nozzles and to obtain preliminary design criteria by testing a number of configurations. Characteristics of interest included low altitude performance, high altitude performance, and the flow transition process. In combination with this performance data, other factors such as cost, weight, fabricability, and vehicle related issues could then be traded to establish the feasibility of the concept.

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BibTeXRIS

Horn, M., Fisher, S.. 1993-11-01. Dual-bell altitude compensating nozzles. https://ntrs.nasa.gov/citations/19940018584

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