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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 />

<strong>the</strong> suit maintained a constant volume when pressurized, enhancing a pilot’s freedom<br />

of movement. Gloves and boots were detachable and zipped to this fabric. The<br />

helmet was joined to <strong>the</strong> suit with a freely-swiveling ring that gave full mobility to<br />

<strong>the</strong> head. Oxygen flowed into <strong>the</strong> helmet; exhalant passed through valves in a neck<br />

seal and pressurized <strong>the</strong> suit. Becker later described it as “<strong>the</strong> first practical full-pressure<br />

suit for pilot protection in space.” 81<br />

Thus accoutered, protected for flight in near-vacuum, X-15 test pilots rode <strong>the</strong>ir<br />

rockets as <strong>the</strong>y approached <strong>the</strong> edge of space and challenged <strong>the</strong> hypersonic frontier.<br />

They returned with results galore for project scientists—and for <strong>the</strong> nation.<br />

X-15: Some Results<br />

During <strong>the</strong> early 1960s, when <strong>the</strong> nation was agog over <strong>the</strong> Mercury astronauts,<br />

<strong>the</strong> X-15 pointed to a future in which piloted spaceplanes might fly routinely to<br />

orbit. The men of Mercury went water-skiing with Jackie Kennedy, but within <strong>the</strong>ir<br />

orbiting capsules, <strong>the</strong>y did relatively little. Their flights were under automatic control,<br />

which left <strong>the</strong>m as passengers along for <strong>the</strong> ride. Even a monkey could do it.<br />

Indeed, a chimpanzee named Ham rode a Redstone rocket on a suborbital flight<br />

in January 1961, three months before Alan Shepard repeated it before <strong>the</strong> gaze of<br />

an astonished world. Later that year ano<strong>the</strong>r chimp, Enos, orbited <strong>the</strong> Earth and<br />

returned safely. The much-lionized John Glenn did this only later. 82<br />

In <strong>the</strong> X-15, by contrast, only people entered <strong>the</strong> cockpit. A pilot fired <strong>the</strong> rocket,<br />

controlled its thrust, and set <strong>the</strong> angle of climb. He left <strong>the</strong> atmosphere, soared high<br />

over <strong>the</strong> top of <strong>the</strong> trajectory, and <strong>the</strong>n used reaction controls to set up his re-entry.<br />

All <strong>the</strong> while, if anything went wrong, he had to cope with it on <strong>the</strong> spot and work<br />

to save himself and <strong>the</strong> plane. He maneuvered through re-entry, pulled out of his<br />

dive, and began to glide. Then, while Mercury capsules were using parachutes to<br />

splash clumsily near an aircraft carrier, <strong>the</strong> X-15 pilot goosed his craft onto Rogers<br />

Dry Lake like a fighter.<br />

All aircraft depend on propulsion for <strong>the</strong>ir performance, and <strong>the</strong> X-15’s engine<br />

installations allow <strong>the</strong> analyst to divide its career into three eras. It had been designed<br />

from <strong>the</strong> start to use <strong>the</strong> so-called Big Engine, with 57,000 pounds of thrust, but<br />

delays in its development brought a decision to equip it with two XLR11 rocket<br />

engines, which had served earlier in <strong>the</strong> X-1 series and <strong>the</strong> Douglas Skyrocket.<br />

Toge<strong>the</strong>r <strong>the</strong>y gave 16,000 pounds of thrust.<br />

Flights with <strong>the</strong> XLR11s ran from June 1959 to February 1961. The best speed<br />

and altitude marks were Mach 3.50 in February 1961 and 136,500 feet in August<br />

1961. These closely matched <strong>the</strong> corresponding numbers for <strong>the</strong> X-2 during 1956:<br />

Mach 3.196, 126,200 feet. 83 The X-2 program had been ill-starred—it had had<br />

two operational aircraft, both of which were destroyed in accidents. Indeed, <strong>the</strong>se<br />

80<br />

The X-15<br />

research aircraft made only 20 flights before <strong>the</strong> program ended, prematurely, with<br />

<strong>the</strong> loss of <strong>the</strong> second flight vehicle. The X-15 with XLR11s thus amounted to X-<br />

2s that had been brought back from <strong>the</strong> dead, and that belatedly completed <strong>the</strong>ir<br />

intended flight program.<br />

The Big Engine, <strong>the</strong> Reaction Motors XLR99, went into service in November<br />

1960. It launched a program of carefully measured steps that brought <strong>the</strong> fall of one<br />

Mach number after ano<strong>the</strong>r. A month after <strong>the</strong> last flight with XLR11s, in March<br />

1961, <strong>the</strong> pilot Robert White took <strong>the</strong> X-15 past Mach 4. This was <strong>the</strong> first time a<br />

piloted aircraft had flown that fast, as White raised <strong>the</strong> speed mark by nearly a full<br />

Mach. Mach 5 fell, also to Robert White, four months later. In November 1961<br />

White did it again, as he reached Mach 6.04. Once flights began with <strong>the</strong> Big<br />

Engine, it took only 15 of <strong>the</strong>m to reach this mark and to double <strong>the</strong> maximum<br />

Mach that had been reached with <strong>the</strong> X-2.<br />

Altitude flights were also on <strong>the</strong> agenda. The X-15 climbed to 246,700 feet in<br />

April 1962, matched this mark two months later, and <strong>the</strong>n soared to 314,750 feet in<br />

July 1962. Again White was in <strong>the</strong> cockpit, and <strong>the</strong> Federation Aeronautique Internationale,<br />

which keeps <strong>the</strong> world’s aviation records, certified this one as <strong>the</strong> absolute<br />

altitude record for its class. A year later, without benefit of <strong>the</strong> FAI, <strong>the</strong> pilot Joseph<br />

Walker reached 354,200 feet. He thus topped 100 kilometers, a nice round number<br />

that put him into space without question or cavil. 84<br />

The third era in <strong>the</strong> X-15’s history took shape as an extension of <strong>the</strong> second one.<br />

In November 1962, with this airplane’s capabilities largely demonstrated, a serious<br />

landing accident caused major damage and led to an extensive rebuild. The new aircraft,<br />

designated X-15A-2, retained <strong>the</strong> Big Engine but sported external tankage for<br />

a longer duration of engine burn. It also took on an ablative coating for enhanced<br />

<strong>the</strong>rmal protection.<br />

It showed anew <strong>the</strong> need for care in flight test. In mid-1962, and for that matter<br />

in 1966, <strong>the</strong> X-2’s best speed stood at 4,104 miles per hour, or Mach 5.92. (Mach<br />

number depends on both vehicle speed and air temperature. The flight to Mach<br />

6.04 reached 4,093 miles per hour.) Late in 1966, flying <strong>the</strong> X-15A-2 without <strong>the</strong><br />

ablator, Pete Knight raised this to Mach 6.33. Engineers <strong>the</strong>n applied <strong>the</strong> ablator<br />

and mounted a dummy engine to <strong>the</strong> lower fin, with Knight taking this craft to<br />

Mach 4.94 in August 1967. Then in October he tried for more.<br />

But <strong>the</strong> X-15A-2, with both ablator and dummy engine, now was truly a new<br />

configuration. Fur<strong>the</strong>r, it had only been certified with <strong>the</strong>se additions in <strong>the</strong> flight<br />

to Mach 4.94 and could not be trusted at higher Mach. Knight took <strong>the</strong> craft to<br />

Mach 6.72, a jump of nearly two Mach numbers, and this proved to be too much.<br />

The ablator, when it came back, was charred and pitted so severely that it could<br />

not be restored for ano<strong>the</strong>r flight. Worse, shock-impingement heating burned <strong>the</strong><br />

engine off its pylon and seared a hole in <strong>the</strong> lower fin, disabling <strong>the</strong> propellant ejec-<br />

81

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