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astronautix.com Highwater


Class: Earth. Type: Atmosphere. Nation: USA.

Release of large quantities of chemicals at high altitudes during suborbital tests of Saturn I.


Specification


Highwater Chronology


25 April 1962 Highwater 1 Launch Site: Cape Canaveral . Launch Vehicle: Saturn I. Duration: 1.62 days.

Second suborbital test of Saturn I. The Saturn SA-2 first stage booster was launched successfully from Cape Canaveral. The rocket was blown up intentionally and on schedule about 2.5 minutes after liftoff at an altitude of 65 miles, dumping the water ballast from the dummy second and third stages into the upper atmosphere. The experiment, Project Highwater, produced a massive ice cloud and lightning-like effects. The eight clustered H-1 engines in the first stage produced 1.3 million pounds of thrust and the maximum speed attained by the booster was 3,750 miles per hour. Modifications to decrease the slight fuel sloshing encountered near the end of the previous flight test were successful.


16 November 1962 Highwater 2 Launch Site: Cape Canaveral . Launch Vehicle: Saturn I. Duration: 1.46 days.

Third suborbital test of Saturn I. Saturn-Apollo 3 (Saturn C-1, later called Saturn I) was launched from the Atlantic Missile Range. Upper stages of the launch vehicle were filled with 23000 gallons of water to simulate the weight of live stages. At its peak altitude of 167 kilometers (104 miles), four minutes 53 seconds after launch, the rocket was detonated by explosives upon command from earth. The water was released into the ionosphere, forming a massive cloud of ice particles several miles in diameter. By this experiment, known as "Project Highwater," scientists had hoped to obtain data on atmospheric physics, but poor telemetry made the results questionable. The flight was the third straight success for the Saturn C-1 and the first with maximum fuel on board.



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Last update 12 March 2001.
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