Propulsion System of DNEPR LV Fourth Stage

Paper number

IAC-05-C4.1.04

Author

Dr. Vladimir Shnyakin, Yuzhnoye State Design Office, Ukraine

Year

2005

Abstract

V. Shnyakin, V. Shul’ga, V. Konokh, A. Zhivotov, V. Koureichik
Yuzhnoye State Design Office
3, Krivorozhskaya, 49008 Dniepropetrovsk, Ukraine
Phone: (38) 0562 384728
E-mail: info@yuzhnoye.com

The report covers further development of works with pneumopump-fed LRE (see report IAC-04-S.1.10 “PNEUMOPUMP-FED LIQUID ROCKET ENGINE TEST RESULTS“ presented in Vancouver in 2004).
The present report involves results of autonomous development of the engine unit with pneumopump feed system started in May 2004 and successfully completed in November 2004. Besides, results of its qualification tests are presented, as well as results of autonomous tests of the feed system including propellant tanks, helium vessels, required valving and pneumopump.

Abstract document

IAC-05-C4.1.04.pdf

Manuscript document

IAC-05-C4.1.04.pdf (🔒 authorized access only).

To get the manuscript, please contact IAF Secretariat.