3000 SHM for a launch of mediumsize spacecraft

  • Slides: 9
Download presentation

3000 SHM for a launch of medium-size spacecraft (Type 1) SHM for a cluster

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

Type 1 of SHM for a launch of medium-size spacecraft 3170 Payload fairing (PLF)

Type 1 of SHM for a launch of medium-size spacecraft 3170 Payload fairing (PLF) Platform B 700 SHM elements 1380 Platform A 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. Adaptor Platform B frame When in orbit, separation of PLF with Platform A occurs 2 seconds prior to SC separation. Protective shield

~ 2600 Modification of SHM (Type 1) enabling the increase in LV lift capability

~ 2600 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. Separated elements

2235 Type 2 of SHM for a launch of several spacecraft PLF upper cone

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

Modification of SHM (Type 2) enabling the increase in LV lift capability Separation of

Modification of SHM (Type 2) enabling the increase in LV lift capability Separation of PLF upper cone 2235 PLF upper cone Separation of GDS 935 PLF lower cone Platform A frame with adaptors 1160 SHM elements Separation of PLF lower cone and Platform A Platform B 920 SHM was designed for the launch of Rapid. Eye 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 Separation of spacecraft Cone with adaptors Separation of spacecraft

Type 3 of SHM for launches of large-size spacecraft 1486 3170 PLF lower cone

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

935 2235 Modification of SHM (Type 3) is prospective SHM for a launch of

935 2235 Modification of SHM (Type 3) is prospective SHM for a launch of large-size SC with extended mass PLF lower cone with GDS 2500 SHM elements Platform A 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. 920 860 Platform B Platform C with adapter Separated elements

~5400 ~4400 Modification of SHM (Type 3) can be used with the adaptor developed

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

Satellite Communication Spacecraft subsystems Spacecraft Spacecraft subsystem overviewSatellite Communication Spacecraft subsystems Spacecraft Spacecraft subsystem overview
Rocket Launch Launch Area Minimum launch areas LaunchRocket Launch Launch Area Minimum launch areas Launch
Simple Harmonic Motion Simple Harmonic Motion SHM SHMSimple Harmonic Motion Simple Harmonic Motion SHM SHM
SPOT Series Launch Date Launch Vehicle Launch LocationSPOT Series Launch Date Launch Vehicle Launch Location
Spacecraft Power Systems Spacecraft Power Systems Power SourceSpacecraft Power Systems Spacecraft Power Systems Power Source
NASA Spacecraft to Mars Challenge NASA Spacecraft DesignNASA Spacecraft to Mars Challenge NASA Spacecraft Design
SPACECRAFT OPERATIONS Paul Collins Head of Spacecraft OperationsSPACECRAFT OPERATIONS Paul Collins Head of Spacecraft Operations
MediumSize Telescope Science Workshop East Asian Core ObservatoriesMediumSize Telescope Science Workshop East Asian Core Observatories