Facing the Heat Barrier - NASA's History Office
Facing the Heat Barrier - NASA's History Office
Facing the Heat Barrier - NASA's History Office
You also want an ePaper? Increase the reach of your titles
YUMPU automatically turns print PDFs into web optimized ePapers that Google loves.
<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mselves superseded,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