23.12.2012 Views

FIRST STEPS TOWARD SPACE - Smithsonian Institution Libraries

FIRST STEPS TOWARD SPACE - Smithsonian Institution Libraries

FIRST STEPS TOWARD SPACE - Smithsonian Institution Libraries

SHOW MORE
SHOW LESS

You also want an ePaper? Increase the reach of your titles

YUMPU automatically turns print PDFs into web optimized ePapers that Google loves.

10 SMITHSONIAN ANNALS OF FLIGHT<br />

the problem of precise and proportional flows of<br />

oxygen and fuel. 31<br />

As early as 1930, REP studied, with the cooperation<br />

of Pierre Montagne, the optimal theoretical<br />

conditions for reaction engine carburation. 32 This<br />

study permitted the determination of the mixture<br />

ratio of liquid oxygen and petroleum ether to<br />

provide optimum performance.<br />

In 1932, REP, at his laboratory on Rue des<br />

Abondances, in Boulogne-sur-Seine, with Montagne<br />

and Salle, attacked the problem of constructing this<br />

reaction engine and developed a test stand at Satory<br />

which enabled him to study, from 1934 to 1937, the<br />

optimum output of his engine by injecting liquid<br />

oxygen and petroleum ether into his graphite combustion<br />

chamber. To deal with problems related to<br />

the use of graphite, REP fabricated a nozzle throat<br />

from tungsten which he smelted in a high-frequency<br />

furnace also specially designed by him for this purpose.<br />

For these works, REP obtained a small contract<br />

from the Direction des ELudes et Fabrications<br />

d'Armements, which assigned Ing^nieur General<br />

Desmazieres to supervise the execution of the<br />

project.<br />

In 1937, for dignitaries visiting REP's laboratory,<br />

the engine operated 60 seconds without incident,<br />

with a thrust of 125 kg. The engine itself met the<br />

qualification standard but the subsidy to enable<br />

REP to construct the gyroscopic stabilization device<br />

that he considered necessary for his rocket was then<br />

refused. REP agreed to study a project for a finned<br />

rocket, without gyroscopic guidance, but he baptized<br />

this the "NIC" for "n'importe comment" and<br />

subsequently abandoned this project. The outbreak<br />

of the 1939 War put an end to REP's activities in<br />

astronautics.<br />

Projects Scorned by Authorities<br />

REP was no doubt the first to recognize the<br />

danger of rockets as weapons capable of intercontinental<br />

ranges, and this worried him. At first<br />

he thought it preferable to remain silent. But the<br />

publicity given by the press to his 1927 work,<br />

"L'Exploration par fusees de la tres haute atmosphere<br />

et la possibility des voyages interplan^taires,"<br />

attracted a large correspondence from which he<br />

learned of works unknown to him: Die Rakete zu<br />

den Planetenraumen by Hermann Oberth (1923); 33<br />

Die Erreichbarkeit der Himmelskorper, by Walter<br />

Hohmann (1925);** and Der Vorstoss in den Weltenraum,<br />

by Max Valier (1925). 35<br />

He began to feel that it had become his duty to<br />

inform the government of his results, of the potential<br />

dangers and the means of developing methods<br />

for sending thousands of tons of projectiles several<br />

hundred miles in a few hours. Using the calculations<br />

he had first made in 1920 with two of his<br />

collaborators, Seal and Marcus, he decided to prepare<br />

a secret report which he sent on 20 May 1928<br />

to his friend, General Ferris, who forwarded it to<br />

his chiefs. 30 This theoretical report demonstrated<br />

that it was already possible to attain a range of<br />

2267 kilometers with an exhaust velocity of 2667<br />

meters per second (REP recognized later that this<br />

estimate was optimistic for the time). In addition,<br />

REP made a detailed study for the particular case<br />

of a rocket of 600-kilometer range, specifying all the<br />

mass ratios, and notably the ballistic yield (the<br />

ratio between the weight of the necessary propellant<br />

and that of the projectile for this range), both for<br />

the mixtures of gasoline and nitrogen peroxide that<br />

he had taken as examples and for the special solid<br />

propellant used by Professor Goddard.<br />

The report ended with economic studies comparing<br />

rocket and aerial bombings and concluded that<br />

long-range rockets would be the artillery of the<br />

future.<br />

After some months, the dossier was returned: it<br />

had aroused absolutely no interest!<br />

No one at the time considered such works apt to<br />

give useful results and the scientist was unable to<br />

overcome the inertia of government officials who<br />

often systematically ignored anything coming from<br />

him.<br />

In 1931 the government nevertheless assigned a<br />

lieutenant of the technical section of the artillery,<br />

J. J. Barre, to work in REP's laboratory. Barre had<br />

been collaborating privately with REP since 1927<br />

and had helped with the calculations for the<br />

memorandum. This assignment lasted only one<br />

year, because it was not considered that "a study of<br />

rockets is worthy of the activity of an officer." In<br />

spite of this precise and prophetic memorandum,<br />

REP did not get the subsidies necessary to carry<br />

out the studies he had proposed.<br />

The situation was different in Germany, where<br />

similar work led to the V-2 rockets. It should<br />

nevertheless be noted that in 1931 Andr^-Louis

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

Saved successfully!

Ooh no, something went wrong!