logo_ua
Desktop EN 2023
logo_ua
logo_ua

12. A Device for Soft Separation of Spacecraft from Launch Vehicle

Organization:

Yangel Yuzhnoye State Design Office, Dnipro, Ukraine

Page: Kosm. teh. Raket. vooruž. 2018 (1); 69-71

DOI: https://doi.org/10.33136/stma2018.01.069

Language: Russian

Annotation: The paper deals with the advantages and peculiarities of operation of a device for soft separation of spacecraft from launch vehicle.

Key words:

Bibliography:
1. Kolesnikov K. S., Kozlov V. I., Kokushkin V. V. Flying Vehicle Stages Separation Dynamics. М., 1977. 221 p.
2. Method of Satellite Separation from Launch Vehicle and Device to Implement the Method: Pat. 108515 Ukraine: MPK В64G1/64 (2006:01) / М. А. Bondar’, V. V. Voloshin, О. М. Duplishcheva, K. F. Mikhailov, V. I. Porubaimekh (Ukraine); applicant and patent holder is Yuzhnoye SDO. No. а201305544; appl. 29.04.13; publ. 12.05.16, Bull. No 9.
Downloads: 19
Abstract views: 
412
Dynamics of article downloads
Dynamics of abstract views
Downloads geography
CountryCityDownloads
Singapore Singapore; Singapore; Singapore; Singapore; Singapore; Singapore; Singapore; Singapore; Singapore9
USA Baltimore; Plano; Monroe; Ashburn; Seattle; Portland; San Mateo; Boardman; Ashburn9
Ukraine Dnipro1
12.1.2018 A Device for Soft Separation of Spacecraft from Launch Vehicle
12.1.2018 A Device for Soft Separation of Spacecraft from Launch Vehicle
12.1.2018 A Device for Soft Separation of Spacecraft from Launch Vehicle
Visits:412