Engineering:Astris (rocket stage)
Astris, the third (upper) stage of the Europa I rocket, on display in Pfaffenwaldring 31 (V 31) on the campus of University of Stuttgart in Vaihingen, Stuttgart, Germany. | |
Manufacturer | ERNO Raumfahrttechnik GmbH |
---|---|
Country of origin | Germany |
Used on | Europa 1 third stage. |
General characteristics | |
Height | 3.36 m (132 in) |
Diameter | 2.00 m (79 in) |
Gross mass | 3,370 kg (7,430 lb) |
Propellant mass | 2,760 kg (6,080 lb) |
Empty mass | 610 kg (1,340 lb) |
Launch history | |
Status | Retired |
Total launches | 4 |
Successes (stage only) | 0 |
Failed | 4 |
Lower stage failed | 0 |
First flight | 1969-07-31 |
Last flight | 1971-11-05 |
Engine details | |
Engines | 1 Astris (rocket engine) |
Thrust | 23.3 kilonewtons (5,200 lbf) |
Specific impulse | 310 s (3.0 km/s) |
Burn time | 330s |
Fuel | Aerozine 50 / N2O4 |
The Astris was an upper stage developed by ERNO Raumfahrttechnik GmbH and MBB as the third stage of the Europa 1 launch vehicle.[1][2][3] It was the Germany contribution to the project and only flew activated four times. The high failure rate of the three and four stage rocket meant that the project was cancelled.[4][5]
On November 29, 1968, its inaugural flight, the Astris third stage exploded.[6][7] On the second attempt on July 1969, the Astris engine failed to start.[6][7] On the third attempt on June 11, 1970, the stage performed correctly, but the fairing failed to separate.[7][6]
On November 5, 1971, the Europa II launched from CSG ELA-1, had a mishap due to structural failure of the third stage.[8][9] After this last failure the project was definitely cancelled.[8]
Details
The stage measured 3.36 m with a diameter of 2 m, and had an empty mass of 610 kg.[4] Propellant (N2O4/Aerozine-50) mass was 2760 kg, and the single Astris engine produced 23.3 kN of thrust.[4]
See also
- Astris (rocket engine)
- Europa (rocket)
- Viking (rocket engine)
References
- ↑ "Propulsion Systems and Launch Vehicles". Deutsches Museum. http://www.deutsches-museum.de/en/exhibitions/transport/astronautics/rocket-engines/. Retrieved 2015-07-25.
- ↑ "Astris engine". http://www.astronautix.com/a/astrisengine.html.
- ↑ "Europa" (in en). https://space.skyrocket.de/doc_lau/europa.htm.
- ↑ 4.0 4.1 4.2 "Astris". http://www.astronautix.com/a/astris.html.
- ↑ Serra, Jean-Jacques. "Europa launchers". http://www.sat-net.com/serra/europa_e.htm. Retrieved 2015-07-25.
- ↑ 6.0 6.1 6.2 "Europa-1" (in en). https://space.skyrocket.de/doc_lau_det/europa-1.htm.
- ↑ 7.0 7.1 7.2 "Europa I". http://www.astronautix.com/e/europai.html.
- ↑ 8.0 8.1 "Europa II". http://www.astronautix.com/e/europaii.html.
- ↑ "Europa-2" (in en). https://space.skyrocket.de/doc_lau_det/europa-2.htm.
Original source: https://en.wikipedia.org/wiki/Astris (rocket stage).
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