Title: EXPERIMENTAL MODEL STUDIES OF THE EFFECTS OF JET FLOWS ON THE LAUNCH VEHICLE AND LAUNCH PAD WITH A SHORT EXHAUST CHANNEL
Abstract:This article presents the results of experimental model studies of gas-dynamic, thermal, and acoustic loads on the elements of a launch vehicle and launch pad when using the CX-36 launch complex with ...This article presents the results of experimental model studies of gas-dynamic, thermal, and acoustic loads on the elements of a launch vehicle and launch pad when using the CX-36 launch complex with a short exhaust channel. The data obtained to date are of significant interest to specialists in the field of space rocket engineering.Read More
Publication Year: 2020
Publication Date: 2020-01-01
Language: en
Type: article
Indexed In: ['crossref']
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