1950-60 Missile / X-Wing Wind Tunnel Model on custom mount

langely wind tunnel sm 01.jpg
langely wind tunnel sm 02.jpg
langely wind tunnel sm 03.jpg
langely wind tunnel sm 04.jpg
langely wind tunnel sm 06.jpg
langely wind tunnel sm 05.jpg
LAL_85428.jpg
original-3.jpg
968px-BeckerTails.jpg
1951-05-4_Charles_McLelland_and_Test_Section.jpg
L-70-2621.jpg
1963_Missles_and_Rockets_Photo.jpg
IMG_2916.jpeg
langely wind tunnel sm 01.jpg
langely wind tunnel sm 02.jpg
langely wind tunnel sm 03.jpg
langely wind tunnel sm 04.jpg
langely wind tunnel sm 06.jpg
langely wind tunnel sm 05.jpg
LAL_85428.jpg
original-3.jpg
968px-BeckerTails.jpg
1951-05-4_Charles_McLelland_and_Test_Section.jpg
L-70-2621.jpg
1963_Missles_and_Rockets_Photo.jpg
IMG_2916.jpeg
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1950-60 Missile / X-Wing Wind Tunnel Model on custom mount

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A quite beautiful model most likely use in the small hypersonic test chamber due to size 8”. The model is machined from aluminum to exacting specs and is mounted in a custom base that was likely done after as a keep sake for display. Stepped base is characteristic of a 50’s type design and there are many test of these types of rockets from the late 50-60’s when hypersonic testing and fin design ‘canard’ placement was tested.

Possible variant in the Becker study group which was the predecessor to the X-15 as many test were created using many possible configurations .

You can see that the model comes apart and the canards can be altered to test out a variety of configurations—a very telling sign that this a precise testing model and you can see another configuration pictured with only two canards.

The greatest contribution made by X-15 operations to the Shuttle program, however, was the energy management procedures that were developed for unpowered X-15 approaches and landings at Edwards. X-15 pilots used the “Drinkwater Approach” that was established by NACA Ames test pilot Fred Drinkwater to make power-off approaches in an aircraft that had a poor lift-to-drag ratio (L/D) and steep glide angle compared to many conventional aircraft. The X-15’s ten-year operational record proved that the Drinkwater Approach could be used safely and reliably. Not long after the conclusion of the X-15 program, when designers of the Shuttle (another low L/D design) realized that their plans to deploy air-breathing engines for approach and landing would be prohibitive in terms of weight and complexity, the X-15’s use of the Drinkwater Approach provided a solution. As X-15 and Shuttle pilot Joe H. Engle noted at the close of the 30-year Shuttle program, "If it were not for the energy management procedures that were demonstrated during the X-15 program, it would have taken longer to proceed with the Space Shuttle...the X-15 allowed us to have confidence that it was not necessary to develop air breathing engines to make the approach and landing task more benign."

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