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  1. B14643 Internet Presentation . mail to: Norbert Brügge

  2. Norbert Brügge, Germany. - Table of contents -. Spacerockets: Database & Analytics. Part 1: Eastern Europe 1. Eastern Europe 2. Eastern Europe 3. China. Japan.

  3. North Korea's long range missile "Hwasong-12" (HS-12) 2 017, May 1 4 -- North Korea has successfully tested its new HS-12 in flight. The new HS-12 missile is not more a mystery. It is a single-stage rocket with a diameter of about 1.50 m.

  4. 20. Feb. 2021 · In a recent question, an answer showed a diagram of a Soviet S5.2/9D21 rocket engine. According to the diagram, there are four pyrocharges (3, 7, 24, and 27) in the engine.

    • Introduction
    • Escape Propulsion
    • In-Space Propulsion
    • Deep Space Propulsion
    • Launch Failures
    • Intensity of Research Activity
    • Future Propulsions
    • Conclusions

    Space flight is undoubtedly a remarkable and probably the most audacious human achievement of the 20thcentury. It started suddenly in the 1950s and grew explosively in the two following decades. During a period of more than fifty years of space flights, many things have changed. The Space Shuttle is a luxury ship compared to the Mercury capsules th...

    According to Caisso et al. (2009)Cassio P, Souchier A, Rothmund C, Alliot P, Bonhomme C, Zinner W, Parsley R, Neill T, Forde S, Starke R, et al. (2009) A liquid propulsion panorama. Acta Astronautica 65(11-12):1723-1737. doi: 10.1016/j.actaastro.2009.04.020 https://doi.org/10.1016/j.actaastro.2009... , in 1898, a Russian schoolteacher, Konstantin T...

    The beginning of the space region that can be characterized as "in-space" propulsion is the point where the launch vehicle upper stage leaves off, and starts performing the functions of primary propulsion, reaction control, station keeping, precision pointing, and orbital maneuvering (Johnson 2012Johnson L (2012) Deputy manager for NASA's advanced ...

    For "deep space" missions, such as missions to the outer planets of our solar system, the propellant energy and mass requirements tend to be higher than for missions closer to Earth due to the higher spacecraft speed required to reduce mission duration, lower solar intensity, maneuvers involved and the generally heavier spacecraft. In many missions...

    Sackheim (2006)Sackheim RL (2006) Overview of United States space propulsion technology and associated space transportation systems, NASA Marshall Space Flight Center, Huntsville, Alabama 35812 JPP -22(6):1310-1332. doi: 10.2514/1.23257 https://doi.org/10.2514/1.23257... researched the causes of launch vehicle failures in the period between 1980 an...

    The number of scientific publications on space propulsion as indexed by Scopus is shown in Fig. 13. As can be seen, the number of publications started to grow significantly after 1993, which sounds as an indicator of the research growth in the field of space propulsion. The same conclusion can be inferred by the growing number of patents, whose gro...

    There are currently some projects under development looking for interesting alternatives to carry humans into the deep space. Such alternatives include some technologies already mentioned, such as solar sail, fusion, plasma, and nuclear propulsion. Table 6presents a short resume of these alternatives, which are all still in a very low TRL (< 3).

    Analyzing the development of space propulsion engines technology over the last fifty years allow us to conclude about a very gradual progress that includes only incremental improvements and differential increases in thrust, specific impulse, weight reduction and fuel efficiency. In a nutshell, we have had just engineering and design gradual improve...

    • Maria Cristina Vilela Salgado, Maria Cristina Vilela Salgado, Mischel Carmen Neyra Belderrain, Tessa...
    • 2018
  5. 6. Jan. 2015 · Norbert Brügge, Germany Contents: Revised: 01.06.2015 R-11 (8A61) R-11M (8K11, Scud-A) R-11MU R-11M Propulsion [PDF] Related documentation Trade Studies Towards an Australian Indigenous Space Launch System

  6. Taepodong-2 ist der Code-Name einer nordkoreanischen Interkontinentalrakete, die auf der Technologie der ebenfalls nordkoreanischen Taepodong-1 basiert. Vereinzelt wird sie auch als No-dong-3, Hwasong -2 oder Moksong -2 bezeichnet. In der Version als Satellitenträgerrakete wird sie von Nordkorea als Unha-2 bezeichnet, eine ...