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Facing the Heat Barrier - NASA's History Office

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<strong>Facing</strong> <strong>the</strong> <strong>Heat</strong> <strong>Barrier</strong>: A <strong>History</strong> of Hypersonics<br />

had taken form with considerable dispatch, and <strong>the</strong> key was <strong>the</strong> feasibility study<br />

of Becker’s group. An independent review at WADC confirmed its conclusions,<br />

whereupon Air Force leaders, both in uniform and in mufti, embraced <strong>the</strong> concept.<br />

Approval at <strong>the</strong> Pentagon <strong>the</strong>n came swiftly.<br />

In turn, this decisiveness demonstrated a willingness to take risks. It is hard today<br />

to accept that <strong>the</strong> Pentagon could endorse this program on <strong>the</strong> basis of just that one<br />

study. Moreover, <strong>the</strong> only hypersonic wind tunnel that was ready to provide supporting<br />

research was Becker’s 11-inch instrument; <strong>the</strong> AEDC hypersonic tunnels<br />

were still several years away from completion. But <strong>the</strong> Air Force was in no mood to<br />

hold back or to demand fur<strong>the</strong>r studies and analyses.<br />

This service was pursuing a plethora of initiatives in jet bombers, advanced fighters,<br />

and long-range missiles. Inevitably, some would falter or find <strong>the</strong>mselves superseded,<br />

which would lead to charges of waste. However, Pentagon officials knew that<br />

<strong>the</strong> most costly weapons were <strong>the</strong> ones that America might need and not have in<br />

time of war. Cost-benefit analysis had not yet raised its head; Robert McNamara<br />

was still in Detroit as a Ford Motor executive, and Washington was not yet a city<br />

where <strong>the</strong> White House would deliberate for well over a decade before ordering <strong>the</strong><br />

B-1 bomber into limited production. Amid <strong>the</strong> can-do spirit of <strong>the</strong> 1950s, <strong>the</strong> X-15<br />

won quick approval.<br />

X-15: The Technology<br />

Four companies competed for <strong>the</strong> main contract, covering design and construction<br />

of <strong>the</strong> X-15: Republic, Bell, Douglas, and North American. Each of <strong>the</strong>m<br />

brought a substantial amount of hands-on experience with advanced aircraft.<br />

Republic, for example, had Alexander Kartveli as its chief designer. He was a highly<br />

imaginative and talented man whose XF-105 was nearly ready for first flight and<br />

whose XF-103 was in development. Republic had also built a rocket plane, <strong>the</strong> XF-<br />

91. This was a jet fighter that incorporated <strong>the</strong> rocket engine of <strong>the</strong> X-1 for an extra<br />

boost in combat. It did not go into production, but it flew in flight tests.<br />

Still, Republic placed fourth in <strong>the</strong> competition. Its concept rated “unsatisfactory”<br />

as a craft for hypersonic research, for it had a thin outer fuselage skin that<br />

appeared likely to buckle when hot. The overall proposal rated no better than average<br />

in a number of important areas, while achieving low scores in Propulsion System<br />

and Tanks, Engine Installation, Pilot’s Instruments, Auxiliary Power, and Landing<br />

Gear. In addition, <strong>the</strong> company itself was judged as no more than “marginal” in<br />

<strong>the</strong> key areas of Technical Qualifications, Management, and Resources. The latter<br />

included availability of in-house facilities and of an engineering staff not committed<br />

to o<strong>the</strong>r projects. 53<br />

Bell Aircraft, ano<strong>the</strong>r contender, was <strong>the</strong> mo<strong>the</strong>r of research airplanes, having<br />

built <strong>the</strong> X-1 series as well as <strong>the</strong> X-2. This firm <strong>the</strong>refore had direct experience<br />

70<br />

The X-15<br />

both with advanced heat-resistant metals and with <strong>the</strong> practical issues of powering<br />

piloted aircraft using liquid-fuel rocket engines. It even had an in-house group that<br />

was building such engines. Bell also was <strong>the</strong> home of <strong>the</strong> designers Robert Woods<br />

and Walter Dornberger, with <strong>the</strong> latter having presided over <strong>the</strong> V-2.<br />

Dornberger’s Bomi concept already was introducing <strong>the</strong> highly useful concept of<br />

hot structures. These used temperature-resistant alloys such as stainless steel. Wings<br />

might be covered with numerous small and very hot metal panels, resembling shingles,<br />

that would radiate heat away from <strong>the</strong> aircraft. Overheating would be particularly<br />

severe along <strong>the</strong> leading edges of wings; <strong>the</strong>se could be water-cooled. Insulation<br />

could protect an internal structure that would withstand <strong>the</strong> stresses and forces of<br />

flight; active cooling could protect a pilot’s cockpit and instrument compartment.<br />

Becker described <strong>the</strong>se approaches as “<strong>the</strong> first hypersonic aircraft hot structures<br />

concepts to be developed in realistic meaningful detail.” 54<br />

Even so, Bell ranked third. Historian Dennis Jenkins writes that within <strong>the</strong> proposal,<br />

“almost every innovation <strong>the</strong>y proposed was hedged in such a manner as to<br />

make <strong>the</strong> reader doubt that it would work. The proposal itself seemed ra<strong>the</strong>r poorly<br />

organized and was internally inconsistent (i.e., weights and o<strong>the</strong>r figures frequently<br />

differed between sections).” 55 Yet <strong>the</strong> difficulties ran deeper and centered on <strong>the</strong><br />

specifics of its proposed hot structure.<br />

Bell adopted <strong>the</strong> insulated-structure approach, with <strong>the</strong> primary structure being<br />

of aluminum, <strong>the</strong> most familiar of aircraft materials and <strong>the</strong> best understood. Corrugated<br />

panels of Inconel X, mounted atop <strong>the</strong> aluminum, were to provide insulation.<br />

Freely-suspended panels of this alloy, contracting and expanding with ease,<br />

were to serve as <strong>the</strong> outer skin.<br />

Yet this concept was quite unsuitable for <strong>the</strong> X-15, both on its technical merits<br />

and as a tool for research. A major goal of <strong>the</strong> program was to study aircraft structures<br />

at elevated temperatures, and this would not be possible with a primary structure<br />

of cool aluminum. There were also more specific deficiencies, as when Bell’s<br />

<strong>the</strong>rmal analysis assumed that <strong>the</strong> expanding panels of <strong>the</strong> outer shell would prevent<br />

leakage of hot air from <strong>the</strong> boundary layer. However, <strong>the</strong> evaluation made <strong>the</strong> flat<br />

statement, “leakage is highly probable.” Aluminum might not withstand <strong>the</strong> resulting<br />

heating, with <strong>the</strong> loss of even one such panel leading perhaps to destructive<br />

heating. Indeed, <strong>the</strong> Bell insulated structure appeared so sensitive that it could be<br />

trusted to successfully complete only three of 13 reference flights. 56<br />

Ano<strong>the</strong>r contender, Douglas Aircraft, had shared honors with Bell in building<br />

previous experimental aircraft. Its background included <strong>the</strong> X-3 and <strong>the</strong> Skyrocket,<br />

which meant that Douglas also had people who knew how to integrate a liquid<br />

rocket engine with an airplane. This company’s concept came in second.<br />

Its design avoided reliance on insulated structures, calling instead for use of a<br />

heat sink. The material was to be a lightweight magnesium alloy that had excellent<br />

71

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