In-depth study of spacecraft service systems and related engineering disciplines for a group of 3 teams (9-12 students in case of sequental study and 18-24 in case of parallel study).

Composition of the kit:

Introsat Constructor. Extension "Mechanical structures". - 3 kits
Introsat Constructor. Satellite power extension. - 3 kits
Introsat Constructor. Extension "Heat and cold in space". - 3 kits
Introsat Constructor. Extension "Magnetism". - 3 kits
Introsat Constructor. Set for assembling a pressure chamber. - 2 kits
Teaching aids on groups of topics "Mechanical structures", "Satellite power", "Heat and cold in space" and "Magnetism"

Information for tenders
OKPD	32.99.53.130
KTRU	32.99.53.130-00000043
What is in box
Groups of themes in education materials	Mechanical structures, Satellite power, Heat and cold in space, Magnetism
Format of education materials	Online
Hardware and materials	Constructor Introsat. Extension "Mechanical structures". - 3 pieces, Constructor Introsat. Satellite Power Extension. - 3 pieces, Constructor Introsat. Expansion "Heat and cold in space". - 3 pieces, Constructor Introsat. Extension "Magnetism". - 3 pieces, Constructor Introsat. Set for assembling a pressure chamber. - 2 pcs, methodical manuals on the topic groups "Mechanical structures", "Satellite power supply", "Heat and cold in space" and "Magnetism"
Box type	Пластиковые контейнеры, пригодные для хранения наборов в лаборатории
Electronic modules features
Space unit type	CubeSat 1U/2U microsatellites (power systems, thermal management, transformation), test benches
Central control unit type	Compatible with: Introsat, Arduino, STM32
Voltage	3.3V, 5V, 9V, adjustable
Power connectors	PLS, JST
Battery type	18650 (2x per power kit)
Data interfaces	I2C (main), GPIO
Data connectors	MicroMatch 4F, PLS
Wireless interfaces	n/a
Education expirience
Themes of lessons	Factors of space flight, designing with load calculations, vibration tests of spacecraft, load-bearing elements of spacecraft structures, deployment of solar batteries, Testing of space technology for operation in conditions of ultra-low pressure, Features of conservation and transfer of heat in the space environment, methods of thermal control of spacecraft, development thermal management systems based on heat pipes, Electricity, Beginnings of circuitry, Voltage converters, Power supply system assembly, Solar panels and their connection diagrams, Spacecraft energy balance
Engineering skills	Programming, Electrical engineering, Circuit engineering (electronic board design), Energy balance calculation, Design, 3D modeling, Strength calculations, SOTR design
Age of students	14 years and older (certain tasks can be adapted for younger children)
Max. amount of students working with 1 kit	9-12 (sequential study), 18-24 (parallel study)
Learning hours	96-126
Competition preparation	Russian National Technological Olympiad (profile "Satellite systems"), program "Planet Watch" (direction "Applied space systems").