S5.142

S5.142
Country of origin Russia
Date 1990-1996
First flight 1996-02-21 (Soyuz TM-23)
Designer KB KhIMMASH
Application attitude control thruster
Predecessor 11D427M
Status Retired
Liquid-fuel engine
Propellant N2O4 / UDMH
Mixture ratio 1.85
Cycle pressure fed
Configuration
Chamber 1
Nozzle ratio 45
Performance
Thrust (vac.) 25 N (5.6 lbf)
Chamber pressure 0.88 MPa (128 psi)
Isp (vac.) 285 s (2.79 km/s)
Burn time 25,000 seconds
Restarts 300,000
Dimensions
Length 180 mm (7.1 in)
Diameter 136 mm (5.4 in)
Dry weight 0.9 kg (2.0 lb)
Used in
KTDU-80
References
References [1][2][3][4][5][6]

The S5.142 (AKA DST-25) is a liquid pressure-fed rocket engine burning N2O4/UDMH with an O/F of 1.85.[1] It is used for crew-rated spacecraft propulsion applications.[5] It was used in KTDU-80 propulsion module from the Soyuz-TM to the Soyuz-TMA-M, as the low thrust thruster (DPO-M).[3] As of the Soyuz MS, KTDU-80 does not uses DPO-M anymore.[6]

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).[1] 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).[1][5]

Versions

This engine has been used in manned Russian space program since the Soyuz TM-23.[1] There are two versions:[4]

See also

References

  1. 1 2 3 4 5 6 "ЖРДМТ от 0,5 кгс до 250 кгс" [Small thrust jet engine from 0.5 kgf to 250 kgf] (in Russian). KB KhIMMASH. Retrieved 2015-07-25.
  2. ↑ "Двигатели 1944-2000: Аавиационные, Ракетные, Морские, Промышленные" [Aviadvigatel 19442-2000: Aviation, rocketry, naval and industry] (PDF) (in Russian). pp. 75–81. Retrieved 2015-07-25.
  3. 1 2 Pillet, Nicolas. "Le système de propulsion du vaisseau Soyouz" [The propulsion system of the Soyuz spacecraft] (in French). Kosmonavtika.com. Retrieved 2015-07-14.
  4. 1 2 3 "Основные двигатели разработки КБХМ" [The main engines produced by KbKhA] (in Russian). Retrieved 2015-07-25.
  5. 1 2 3 RKK Energia (June 1999). "3.17. Комбинированная Двигательная Установка (КДУ) (Combined Propulsion System)". Soyuz Crew Operations Manual (SoyCOM) (ROP-19) Final. NASASpaceFlight.com. pp. 122–129. (subscription required (help)).
  6. 1 2 Zak, Anatoly (2016-07-07). "Propulsion system for the Soyuz MS spacecraft". Russian Space Web. Retrieved 2016-07-06.


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