01.07.2014 Views

Exploring the Unknown: Selected Documents in ... - The Black Vault

Exploring the Unknown: Selected Documents in ... - The Black Vault

Exploring the Unknown: Selected Documents in ... - The Black Vault

SHOW MORE
SHOW LESS

Create successful ePaper yourself

Turn your PDF publications into a flip-book with our unique Google optimized e-Paper software.

<strong>Explor<strong>in</strong>g</strong> <strong>the</strong> <strong>Unknown</strong><br />

51<br />

is determ<strong>in</strong>ed only by entry speed and flight-path angle, provided this deceleration<br />

occurs before impact. This provision is satisfied by missiles presently of more<br />

usual <strong>in</strong>terest.<br />

<strong>The</strong> results of <strong>the</strong> motion analysis are employed to determ<strong>in</strong>e means available<br />

to <strong>the</strong> designer for m<strong>in</strong>imiz<strong>in</strong>g aerodynamic heat<strong>in</strong>g. Emphasis is placed upon<br />

<strong>the</strong> convective-heat<strong>in</strong>g problem <strong>in</strong>clud<strong>in</strong>g not only <strong>the</strong> total heat transfer but also<br />

<strong>the</strong> maximum average and local rates of heat transfer but also <strong>the</strong> maximum average<br />

and local rates of heat transfer per unit area. It is found that if a missile is<br />

so heavy as to be retarded only slightly by aerodynamic drag, irrespective of <strong>the</strong><br />

magnitude of <strong>the</strong> drag force, <strong>the</strong>n convective heat<strong>in</strong>g is m<strong>in</strong>imized by m<strong>in</strong>imiz<strong>in</strong>g<br />

<strong>the</strong> total shear force act<strong>in</strong>g on <strong>the</strong> body. This condition is achieved by employ<strong>in</strong>g<br />

shapes with a low pressure drag. On <strong>the</strong> o<strong>the</strong>r hand, if a missile is so light as<br />

to be decelerated to relatively low speeds, even if acted upon by low drag forces,<br />

<strong>the</strong>n convective heat<strong>in</strong>g is m<strong>in</strong>imized by employ<strong>in</strong>g shapes with a high pressure<br />

drag, <strong>the</strong>reby maximiz<strong>in</strong>g <strong>the</strong> amount of heat delivered to <strong>the</strong> atmosphere and<br />

m<strong>in</strong>imiz<strong>in</strong>g <strong>the</strong> amount delivered to <strong>the</strong> body <strong>in</strong> <strong>the</strong> deceleration process. Blunt<br />

shapes appear superior to slender shapes from <strong>the</strong> standpo<strong>in</strong>t of hav<strong>in</strong>g lower<br />

maximum convective heat-transfer rates <strong>in</strong> <strong>the</strong> region of <strong>the</strong> nose. <strong>The</strong> maximum<br />

average heat-transfer rate per unit area can be reduced by [2] employ<strong>in</strong>g<br />

ei<strong>the</strong>r slender or blunt shapes ra<strong>the</strong>r than shapes of <strong>in</strong>termediate slenderness.<br />

Generally, <strong>the</strong> blunt shape with high pressure drag would appear to offer considerable<br />

promise of m<strong>in</strong>imiz<strong>in</strong>g <strong>the</strong> heat transfer to missiles of <strong>the</strong> sizes, weights,<br />

and speeds presently of <strong>in</strong>terest.<br />

Document I-3<br />

Document Title: Adelbert O. Tischler, Head, Rocket Combustion Section, NACA,<br />

Memorandum for Associate Director, NACA, “M<strong>in</strong>imum Man-In-Space Proposals<br />

Presented at WADC, 29 January 1958 to 1 February 1958,” 10 April 1958.<br />

Source: Folder 18674, NASA Historical Reference Collection, NASA History<br />

Division, NASA Headquarters, Wash<strong>in</strong>gton DC.<br />

Document I-4<br />

Document Title: Paul E. Purser, Aeronautical Research Eng<strong>in</strong>eer, NACA, Memorandum<br />

for Mr. Gilruth, “Langley Manned-Satellite Program,” 11 April 1958.<br />

Source: Folder 18674, NASA Historical Reference Collection, NASA History<br />

Division, NASA Headquarters, Wash<strong>in</strong>gton, DC.<br />

<strong>The</strong> spr<strong>in</strong>g of 1958 brought to <strong>the</strong> fore a range of possibilities for advocates of an aggressive<br />

spaceflight effort <strong>in</strong> <strong>the</strong> U.S. <strong>The</strong> Soviet successes with Sputniks I and II <strong>in</strong> <strong>the</strong> fall of 1957,<br />

coupled with <strong>the</strong> spectacular failure of a televised Vanguard launch on 6 December 1957,<br />

ensured that national leaders were under <strong>the</strong> gun to take positive action. Accord<strong>in</strong>gly, this<br />

situation led directly to several efforts aimed at “catch<strong>in</strong>g up” to <strong>the</strong> Soviet Union’s space

Hooray! Your file is uploaded and ready to be published.

Saved successfully!

Ooh no, something went wrong!