Skyroot Aerospace Flags Off Vikram-1 Payload Fairing

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Skyroot Aerospace Flags Off Vikram-1 Payload Fairing

Science & Technology
Skyroot Aerospace Flags Off Vikram-1 Payload Fairing

Skyroot Aerospace flags off the payload fairing of Vikram-1, marking the beginning of its launch campaign. The development is relevant for India’s private space sector and private orbital satellite launches.

Vikram-1 Launch Vehicle:

Dimension Key Details
Rocket Type Vikram-1 is India’s first privately developed multi-stage orbital launch vehicle authorised by IN-SPACe.
Developer Vikram-1 is developed by Skyroot Aerospace, a private company.
Skyroot Milestone Skyroot Aerospace is the first private company to carry out a single-stage sub-orbital flight in 2022.
Launch Site The launch site is Satish Dhawan Space Centre, Sriharikota.
Launch Vehicle Type Vikram-1 is a multi-stage launch vehicle using solid, liquid, and cryogenic propulsion.
Height Vikram-1 is approximately 23 metres high, equivalent to a 7-storey building.
Name The launch vehicle is named to honour Dr Vikram Sarabhai, considered the father of the Indian space programme.
Propulsion Systems The propulsion systems are named after Indian scientific pioneers: Kalam for high-thrust solid boosters, Raman for liquid engines, and Dhawan for the cryogenic stage.
Payload Capacity Vikram-1 carries up to 350 kg to Low Earth Orbit and 260 kg to Sun-synchronous Orbit.
Structure The structure is made of carbon composite instead of metals, making it lightweight, faster to assemble, and cost-effective.
3D-Printed Engines The engines are indigenously developed and 3D-printed to reduce manufacturing time and simplify assembly.
Launch Flexibility Vikram-1 provides for dedicated launches, rideshare launches, and custom orbital deployment.
Low Earth Orbit Low Earth Orbit has an altitude range of 160–2,000 km and is used for communication constellations, ISS, and general Earth observation.
Sun-Synchronous Orbit Sun-synchronous Orbit has an altitude range of 500–800 km, near-polar inclination of 97°–99°, and is used for remote sensing, cartography, weather, and environmental monitoring.
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Attempt Possible Qs

Q 1 / 2

Consider the following statements about Vikram-1:

1. It is a multi-stage orbital launch vehicle.
2. It uses solid, liquid, and cryogenic propulsion.
3. It is described as India’s first privately developed orbital launch vehicle authorised by IN-SPACe.

Which of the statements given above are correct?