To install click the Add extension button. That's it.

The source code for the WIKI 2 extension is being checked by specialists of the Mozilla Foundation, Google, and Apple. You could also do it yourself at any point in time.

4,5
Kelly Slayton
Congratulations on this excellent venture… what a great idea!
Alexander Grigorievskiy
I use WIKI 2 every day and almost forgot how the original Wikipedia looks like.
Live Statistics
English Articles
Improved in 24 Hours
Added in 24 Hours
Languages
Recent
Show all languages
What we do. Every page goes through several hundred of perfecting techniques; in live mode. Quite the same Wikipedia. Just better.
.
Leo
Newton
Brights
Milds

Astris (rocket stage)

From Wikipedia, the free encyclopedia

Astris
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.
ManufacturerERNO Raumfahrttechnik GmbH
Country of originGermany
Used onEuropa 1 third stage.
General characteristics
Height3.36 m (132 in)
Diameter2.00 m (79 in)
Gross mass3,370 kg (7,430 lb)
Propellant mass2,760 kg (6,080 lb)
Empty mass610 kg (1,340 lb)
Launch history
StatusRetired
Total launches4
Successes
(stage only)
0
Failed4
Lower stage
failed
0
First flight1969-07-31
Last flight1971-11-05
Engine details
Powered by1 Astris (rocket engine)
Maximum thrust23.3 kilonewtons (5,200 lbf)
Specific impulse310 s (3.0 km/s)
Burn time330s
PropellantAerozine 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 German 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

References

  1. ^ "Propulsion Systems and Launch Vehicles". Deutsches Museum. Retrieved 2015-07-25.
  2. ^ "Astris engine". www.astronautix.com. Retrieved 2023-10-10.
  3. ^ "Europa". Gunter's Space Page. Retrieved 2023-10-10.
  4. ^ a b c "Astris". www.astronautix.com. Retrieved 2023-10-10.
  5. ^ Serra, Jean-Jacques. "Europa launchers". Retrieved 2015-07-25.
  6. ^ a b c "Europa-1". Gunter's Space Page. Retrieved 2023-10-10.
  7. ^ a b c "Europa I". www.astronautix.com. Retrieved 2023-10-10.
  8. ^ a b "Europa II". www.astronautix.com. Retrieved 2023-10-10.
  9. ^ "Europa-2". Gunter's Space Page. Retrieved 2023-10-10.


This page was last edited on 10 October 2023, at 16:52
Basis of this page is in Wikipedia. Text is available under the CC BY-SA 3.0 Unported License. Non-text media are available under their specified licenses. Wikipedia® is a registered trademark of the Wikimedia Foundation, Inc. WIKI 2 is an independent company and has no affiliation with Wikimedia Foundation.