
SS AMU SAT
A Students' Satellite Initiative
About
The SS AMU SAT project is an initiative by the Students and Alumni of Zakir Husain College of Engineering and Technology. The project was concieved during a discussion among a small group of students and alumni during the Winters of 2021, at the AMU RoboClub.
Finally, in the early week of December, 2021, this project kick-started after everal rounds of discussions. It is pertinent to mention that there has also been an observation of the NAAC committee, that visited in December 2021, to innovate in the area of Aerial Technology; and thus, the timing of this project could never have been more suited.
In the weeks to come, the team grew from a handful to a dozen, to design the following subsystems:Electrical Power System Payload Attitude Determination and Control System Communication Systems
Many alumni have been called in for help and guidance. Experts from ISRO and people with prior experience in satellite design have been helping to make this project a success, and eventually commissioning in the Lower Earth Orbit (LEO).
Objective
The vision of SS AMU SAT is to raise awareness and educate the students in the field of Space Technology and create an ecosystem for Satellite Development.
The primary objective of this is to demonstrate a Novel Image Compression Technique to establish a faster multimedia transmission. Additionally, the project aims to monitor the economic growth of our Nation using Satellite Imagery and a novel machine learning algorithm. The acquired data shall be compared with the existing economic data available on public domain and any deviation will be duly evaluated and reported. This system shall bridge the gap between theoritical implementation and the actual outcome of economic policies. It is planned to make all the raw data available in public domain for researchers, economists and data scientists.
In addition to the above, this project shall also serve as a platform to test the in-house built components such as - ADCS Bus, Payload Bus, EPS Bus and the 3U Satellite Bus.
Prof. Sufyan Beg
Principal
Zakir Husain College of Engg. & Technology
Prof. Ekram Khan
Chairman
Dept. of Electronics Engg., ZHCET
Project In-charge
Prof. Saleem Anwar Khan
Professor
Dept. of Mechanical Engg., ZHCET
Dr. Mohammad Sharique
Assistant Professor
Dept. of Electronics Engg., ZHCET
Dr. Adil Sarwar
Assistant Professor
Dept. of Electrical Engg., ZHCET
Mr. Ateeb Ahmad
Assistant Professor
Dept. of Mechanical Engg., ZHCET
Mr. Raunaque Qaiser
Gr. Manager
ST Microelectronics
Dr. Nazeer Ahmad
Scientist
ISRO
Dr. Abdullah Amir Hayat
Post-Doc Fellow
SUTD, Singapore
Mr. Faraz Ahmad
Dy. Manager
NHDC Limited
Project Mentor
Mr. Ishrat Jamal
Scientist
ISRO
Mr. Ghulam Sarwar
Scientist
ISRO
Mr. Mohammad Talha
Engineer
NXP
Mr. Monis Khan
Scientist
ISRO
- Ms. Ilma Shah
- Mr. Ahsan Waseem
- Mr. Mohd Azhan
- Ms. Tanu Attri
- Mr. Kanuj Chitranshu
- Ms. Poorti Varshney
- Ms. Munira Sultan
- Ms. Atifa Saeed
- Mr. Humam Zamir
- Mr. Amzar Faisal
- Mr. Inayat Rasool
- Mr. Mohammad Suhaib, B.Sc. (Phy.)
- Mr. Mohammad Afzal
- Mr. Syed Kashan Raza
- Ms. Tahreem Zaidi, M.Tech. (Comm.)
- Ms. Tarannum Zafar Ansari
- Mr. Azhan Kamil
- Ms. Kulsum Iliyas
- Mr. Anant Agrawal
- Mr. Abdul Hadi
- Mr. Tarun Singh
- Mr. Rayyan Tirmizi
- Ms. Mansha Kazmi
- Ms. Areesha Usmani
- Business Head,
Big Basket, Mumbai
- C.O.O.,
KP Group, Surat
- Senior Integration Architect
Macquarie Group, Australia
Features. The nameplate of our spacecraft.
Small | Light | Beautiful
Name | SS AMU SAT |
CubeSat Size | 3U |
Dimensions | 300mm X 100mm X 100mm |
Weight | ~3500 gm |
Type of Orbit | Circular Polar Orbit in LEO |
Power | Solar and Battery powered |
Attitude Correction | Available with Magneto-torquers and Reaction Wheels |
Payload | On-board Camera |
Communication System | Beacon on VHF, UPLINK and DOWNLINK on UHF/ S-Band |
Chassis Material | Aluminum |
Progress
We are nearly there, have a look!
The preliminary designing has nearly ended. Thanks to the experts aroud the globe who have helped to realise our ideas.
RECENT UPDATES:
Orbit. The final destination!
Polar | Lower Earth Orbit
Semi Major Axis | 6884.75 m |
Eccentricity | 0 |
Inclination | 60.69 deg |
Argument of Perigee | 0 deg |
RAAN | 284.457 deg |
True Anomaly | 0 deg |
Orbit Altitude | 506.75 km |
Orbital Velocity | 7.60887 km/s |
Orbital Period | 1hr 34min 45sec (94.75 min) |
Ground Track Repetition | 15.48 times in 24 hrs |
We are not there yet! But we know how it will look.
A simulation of the spacecraft in the orbit.
Fundings
Respected Visitor,
Thank You for your interest, and we appreciate the time that you have taken to go through our website. The estimated expenditure for the design, fabrication, assembly, testing, validation, space qualification, launch and commissioning of SS AMU SAT falls in the tune of nearly INR 45.0 Lakhs (including estimated launch cost). So far, the students have managed to run this project with their own contributions. We have obtained the estimate through the FAQ published by the 75 Student Satellite Programme initiated by the ITCA. However, the members have been trying to manufacture the components in-house so as to bring down the overall cost.
Considering the total requirement, it is evident that the small pool of students' contribution will not be sufficient to launch our project into Space. In view of this, generous contribution is requested from all to help us realise this project.
The bank account details for donations shall be updated very soon on the website.
Monetory contributions are welcome and we would also appreciate your kind efforts to procure the intended items. The brochure is available here. The list of components that we are intending to buy is available with the Project Incharge (Prof. Ekram Khan | ekhan.el@amu.ac.in) and Project Mentor (Mr. Faraz Ahmad | imfarazahmad@gmail.com). Alternatively, for our dearest contributers who wish to make monetory donations, we shall provide the account details upon request.
The interested contributers may e-mail their contact informations to the Project In-charge or Project Mentor as mentioned below. The list of required components and equipment shall be notified along with the link to online stores.
List of Contributors
Mr. Mohammad Saif
Business Head
BigBasket, Mumbai
Mr. Shaheedul Hasan
C.O.O.
KP Group, Surat
Mr. Sarfraz Khan
Senior Integration Architect
Macquarie Group, Australia