Measurements of the Progress-M main engine retrofiring plume at orbital conditions

Author:

Karabadzhak G.1,Plastinin Yu.1,Afanasiev A.1,Szhenov E.1,Drakes J.2,McGregor W.2,Nichols J.2,Reed R.2,Bradley D.3,Teslenko V.4,e al

Affiliation:

1. TsNIIMASH, Korolev, Russia

2. Sverdrup Technology, Inc., AEDC Group, Arnold AFB, TN

3. USAF, Arnold AFB, TN

4. RSC Energia, Korolev, Russia

Publisher

American Institute of Aeronautics and Astronautics

Reference9 articles.

1. O(1S) 557.7 nm and O(1D) 630 nm emissions in shuttle thruster plumes

2. The interaction of the atmosphere with the space shuttle thruster plume: The NH(A-X) 336-nm emission

3. Karabadzhak, G. F., Plastinin, Yu., Khmelinin, B., Teslenko, V., Shvets, N., Drakes, J. A., Swann, D. G., and McGregor, W. K. "Experimentation Using the Mir Station as a Space Laboratory," AIAA Paper 98-0288, 36* Aerospace ences Meeting & Exhibit, Reno NV, Januaryl998.

4. Exhaust Plume." 37th Aerospace Sciences Meeting Exhibit, Reno, NV, January 1999. & AIAA-99-1042

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