various types of space head module shm for a launch of large-size spacecraft (type 3) shm for a...
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Various Types of Space Head Module
SHM for a launch of large-size
spacecraft (Type 3)SHM for a cluster launch of several
spacecraft (Type 2)SHM for a launch of medium-size spacecraft
(Type 1)
5250
~ 4
500
5250
~ 1
300
~ 1
300
7450
~54
00
3000
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Type 1 of SHM for a launch of medium-size spacecraft
Payload fairing (PLF)
Platform A
Platform B
Adaptor
Platform B frame
Protective shield
SHMelements
When in orbit, separation of PLF with Platform A occurs 2 seconds prior to SC separation.
SHM was used for the launches of Genesis-1, 2 spacecraft. Its modification with a different adaptor was used for the launch of OICETS and INDEX spacecraft. SHM can be used with many variants of adaptor.
700
3170
1380
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Modification of SHM (Type 1) enabling the increase in LV lift capability
SHM was designed for the launch of Theos spacecraft. It can be used with many variants of adaptors.
~ 2
600
Separated elements
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SHM elements
PLF upper cone
Platform A with dispensers
Platform A
Adaptor and Platform B frame
Most popular type of SHM to be used for launching several spacecraft.
PLF lower cone
Gas-Dynamic Shield (GDS)
Platform B
Type 2 of SHM for a launch of several spacecraft
Separated elements
2235
935
700
1380
~ 1
300
~ 1
800
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PLF upper cone
Platform A frame with adaptors
Platform A
Cone with adaptors
SHMelements
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
PLF lower cone
GDS
Platform B
Separation of PLF upper cone
Separation of GDS
Separation of PLF lower cone and Platform A
Separation of spacecraft
Separation of spacecraft
Modification of SHM (Type 2) enabling the increase in LV lift capability
2235
935
920
1160
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Type 3 of SHM for launches of large-size spacecraft
PLF
PLF lower cone with GDS
Platform A
Platform B
Adaptor
SHMelements
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.
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.
3170
1486
2260
2020
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Modification of SHM (Type 3) is prospective SHM for a launch of large-size SC with extended mass
PLF
PLF lower cone with GDS
Platform A
Platform B
Platform C with adapter
SHM elements
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. Separated elements
2235
935
860
2500
920
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Modification of SHM (Type 3) can be used with the adaptor developed for a launch of TerraSAR-X SC
Using of the adaptor developed for a launch of TerraSAR-X SC allows to extend payload envelope
~54
00~44
00