E-1 (rocket)

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E-1
1-пуску-посвящается 1S.jpg
Replica E-1
Typesounding rocket
Place of originReykani Socialist Republic
Production history
Produced10 May, 1957
Specifications
Mass13,430 kg (29,610 lb)
Length14,650 mm (48 ft 1 in)
Diameter1,650 mm (5 ft 5 in)

EngineLiquid rocket engine
27,200 kgf (267,000 N; 60,000 lbf)
Wingspan3,560 mm (11 ft 8 in)
Propellant
Operational
range
270 km (170 mi)
Accuracy5 km

The E-1 rocket was a sounding rocket, the first manufactured in the Reykani Socialist Republic. The rocket is a close copy of other sounding rockets from major powers but never entered full production since only two were ever built. Nevertheless, production and launching of the E-1 gave the Reykanes valuable experience which later enabled them to construct its own much more capable rockets. The E-1 project launched two rockets between 25 April, 1957 and 13 May, 1957. All were launched from the Höfðanátfari Air Base.


History

The first E-1 rocket is transported to the launch site on a truck trailer. It was launched on 25 April, 1957 from the Höfðanátfari Air Base

Launch history

E-1 was launched two times in 1957.

List of E-1 launches
Designation Date Launch site Remarks Image
E-1 "Hamarhákarlar" 22 April 1957 Höfðanátfari Air Base succesfull launch but engine cut out after reaching about 100 m Bundesarchiv RH8II Bild-B2055-44, Peenemünde, Raketenrampe mit V2.jpg
E-1 "Sagskötur" 13 May, 1957 Höfðanátfari Air Base reached 100 kilometres (62 mi), the boundary of space Bundesarchiv Bild 141-1880, Peenemünde, Start einer V2.jpg

First launch

The E-1 "Hamarhákarlar" was the first rocket, which was produced in 22 April 1957 and launched 3 days later on 25 April.

Second launch

Description and development

Drawing of the Reykani E-1 rocket

Though the E-1 was a close copy of other rocket designs during the era, it was ultimately considerably less reliable than its template since it was a expensive project and due to not knowing all details. The rocket was 14,650 mm (577 in) in length and weighing 13.5 tons. 50  9.2 tons of the E-1's mass was devoted to propellant: 4 tons of ethyl alcohol and 5 tons of liquid oxygen, which fed the Reykani-designed RD-100 engine. It was noted that the E-1 rocket could carry a 785-kilogram (1,731 lb) warhead of conventional explosive to a maximum range of 270 kilometres (170 mi), with an accuracy of about 5 kilometres (3.1 mi).

WORK IN PROGRESS