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Space Head Modules of Dnepr LV

Space Head Modules of Dnepr LV. Space Head Modules of Dnepr LV. Various Types of Space Head Module. ~ 1300. ~5400. 7450. 5250. 5250. ~ 4500. ~ 1300. 3000. SHM for a launch of large-size spacecraft ( Type 3). SHM for a cluster launch of several spacecraft (Type 2).

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Space Head Modules of Dnepr LV

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  1. Space Head Modules of Dnepr LV Space Head Modules of Dnepr LV

  2. Various Types of Space Head Module ~ 1300 ~5400 7450 5250 5250 ~ 4500 ~ 1300 3000 SHM fora launch of large-size spacecraft (Type 3) SHM fora cluster launch of several spacecraft(Type 2) SHM for a launch of medium-size spacecraft (Type 1)

  3. Type 1 of SHM for a launch of medium-size spacecraft Payload fairing (PLF) 3170 PlatformA 1380 SHM elements Platform B 700 Adaptor SHM was used for the launches of Genesis-1, 2 spacecraft. Its modification with a different adaptor was used for the launch of OICETSand INDEX spacecraft. SHM can be used with many variants of adaptor. Platform B frame When in orbit, separation of PLF with Platform A occurs 2 seconds prior to SC separation. Protective shield

  4. Modification of SHM (Type 1)enabling the increase in LV lift capability ~ 2600 SHM was designed for the launch of Theos spacecraft. It can be used with many variants of adaptors. Separated elements

  5. Type 2 of SHM for a launch of several spacecraft PLF upper cone 2235 Gas-Dynamic Shield (GDS) PLF lower cone 935 ~ 1300 Platform A with dispensers SHM elements Platform A ~ 1800 1380 Platform B 700 Most popular type of SHM to be used for launching several spacecraft. Separated elements Adaptor and Platform B frame

  6. Modification of SHM (Type 2) enabling the increase in LV lift capability Separation of PLF upper cone PLF upper cone 2235 Separation of GDS GDS Separation of spacecraft PLF lower cone 935 Separation of PLF lower cone and Platform A Platform A frame with adaptors SHM elements Platform A 1160 Platform B Separation of spacecraft SHM was designed for the launch of RapidEye spacecraft. LV fitted with this SHM possesses highest lift capability due to use of a lighter shells of Platform A and Platform B newly manufactured 920 Cone with adaptors

  7. Type 3 of SHM for launches of large-size spacecraft PLF 3170 PLF lower cone with GDS 1486 Platform A SHM elements 2020 Platform B 2260 SHM was designed for the launch of TerraSAR-X spacecraft. To be used for the launches of Tandem-Х, Kompsat-5 and CryoSat-2 spacecraft. Adaptor PLF is jettisoned at final phase of 2nd stage operation. When in orbit, separation of Platform A with GDS occurs 2 seconds prior to SC separation.

  8. Modification of SHM (Type 3) is prospective SHM for a launch of large-size SC with extended mass 2235 PLF PLF lower cone with GDS 935 SHM elements Platform A 2500 Platform B 860 Prospective SHM with extended payload envelope for a launch of large-size SC with extended mass. New type of PLF lower cone was manufactured to extend the payload envelope. Platform C with adapter 920 Separated elements

  9. Modification of SHM (Type 3) can be used with the adaptor developed for a launch of TerraSAR-X SC ~4400 ~5400 Using of the adaptor developed for a launch of TerraSAR-X SC allows to extend payload envelope

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