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- Q20982786 subject Q20829258.
- Q20982786 subject Q21412544.
- Q20982786 subject Q7142278.
- Q20982786 abstract "The S5.142 (AKA DST-25) is a liquid pressure-fed rocket engine burning N2O4/UDMH with an O/F of 1.85. It is used for crew-rated spacecraft propulsion applications. It is currently used in the Soyuz-TMA-M spacecraft propulsion module KTDU-80, as the low thrust thruster (DPO-M).The S5.142 generates 25 N (5.6 lbf) of thrust with a chamber pressure of 0.88 MPa (128 psi) and a nozzle expansion of 45 that enables it to achieve a specific impulse of 285 s (2.79 km/s). It is rated for 300,000 starts with a total firing time of 25,000 seconds and can do single burns from 0.03seconds to 4,000 seconds. Each unit weights 0.9 kg (2.0 lb).".
- Q20982786 wikiPageExternalLink main.php?id=53.
- Q20982786 wikiPageWikiLink Q159.
- Q20982786 wikiPageWikiLink Q161296.
- Q20982786 wikiPageWikiLink Q190795.
- Q20982786 wikiPageWikiLink Q20744072.
- Q20982786 wikiPageWikiLink Q20829258.
- Q20982786 wikiPageWikiLink Q21412544.
- Q20982786 wikiPageWikiLink Q2425489.
- Q20982786 wikiPageWikiLink Q2705481.
- Q20982786 wikiPageWikiLink Q287464.
- Q20982786 wikiPageWikiLink Q335225.
- Q20982786 wikiPageWikiLink Q382984.
- Q20982786 wikiPageWikiLink Q4206307.
- Q20982786 wikiPageWikiLink Q4231574.
- Q20982786 wikiPageWikiLink Q51504.
- Q20982786 wikiPageWikiLink Q530600.
- Q20982786 wikiPageWikiLink Q609089.
- Q20982786 wikiPageWikiLink Q624622.
- Q20982786 wikiPageWikiLink Q7142278.
- Q20982786 wikiPageWikiLink Q748738.
- Q20982786 wikiPageWikiLink Q752783.
- Q20982786 wikiPageWikiLink Q83001.
- Q20982786 wikiPageWikiLink Q860308.
- Q20982786 comment "The S5.142 (AKA DST-25) is a liquid pressure-fed rocket engine burning N2O4/UDMH with an O/F of 1.85. It is used for crew-rated spacecraft propulsion applications. It is currently used in the Soyuz-TMA-M spacecraft propulsion module KTDU-80, as the low thrust thruster (DPO-M).The S5.142 generates 25 N (5.6 lbf) of thrust with a chamber pressure of 0.88 MPa (128 psi) and a nozzle expansion of 45 that enables it to achieve a specific impulse of 285 s (2.79 km/s).".
- Q20982786 label "S5.142".
- Q20982786 homepage main.php?id=53.