Aagaman: India's First Privately Built Orbital Rocket Reaches the Pad
UPSC-standard MCQs with explanations, trap analysis, and approach guide. Answer after the test — not before.
1
Easy
1
Medium
1
Hard
Practice this set
3 questions · full analysis after submission · no sign-up required
Article summary
Skyroot Aerospace's Vikram-1, India's first privately developed orbital-class launch vehicle, has been prepared for its maiden flight — a mission named Aagaman, Sanskrit for 'arrival' — scheduled for 18 July 2026 from ISRO's launch complex at Sriharikota. The vehicle stands roughly 20 metres tall with a diameter of 1.7 metres and uses four stages: the first three solid-propellant, and a fourth liquid stage powered by 3D-printed Raman engines for orbital insertion and precise manoeuvring. Its structure is all-carbon composite, and it is designed to carry about 350 kg to low Earth orbit or 260 kg to a sun-synchronous orbit, with customer payloads on this flight to be deployed at roughly 450 km. The design philosophy is deliberately unglamorous — simplicity, reliability and the ability to assemble and launch within 24 hours — aimed squarely at the small-satellite market where operators want schedule control rather than maximum lift. Success would make India the third country, after the United States and China, with a private company capable of orbital launch. Skyroot previously flew Vikram-S in 2022, a suborbital demonstration; reaching orbit is a substantially harder problem, requiring not altitude but the velocity to stay up.
What this tests
Sample questions — answers revealed after test
Q1. With reference to India's space sector reforms, which one of the following statements is correct?
Q2. Skyroot flew the suborbital Vikram-S in 2022 and now attempts orbital flight with Vikram-1. Which one of the following best explains why orbital flight is a substantially harder problem?
Q3. Consider the following statements regarding Vikram-1: 1. It stands about 20 metres tall with a diameter of 1.7 metres, has an all-carbon composite structure, and comprises four stages of which the first three are solid-propellant. 2. It can place roughly 350 kg into low Earth orbit or 260 kg into sun-synchronous orbit, with maiden-flight payloads to be deployed at about 450 km. 3. Success would make India the first country in the world to achieve private orbital launch capability. Which of the statements given above are correct?