What makes Skyroot’s Vikram-1 launch unique? | Explained

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Skyroot’s Vikram-1 has made India only the third country where a private company has independently placed payloads in orbit. Here’s what makes the mission significant

Updated - July 18, 2026 04:40 pm IST

This photograph taken on July 7, 2026 shows a Vikram-S rocket model at Skyroot Aerospace facility on the outskirts of Hyderabad. | Photo Credit: AFP

The story so far: The Vikram-1 rocket, built by the Hyderabad firm Skyroot, shot through the sky a little past noon on July 18, 2026. The seven-storey rocket lifted off ISRO’s First Launch Pad at Sriharikota and, a little over fifteen minutes later, placed its payloads in an orbit roughly 450 km above the earth. The rocket was Aerospace, and the mission — named Aagaman, Sanskrit for “arrival” — made India only the third country, after the United States and China, whose private industry can reach orbit on its own launch vehicle.

Skyroot’s 3D-printed engine: What it is and why it matters

Rocket engines have traditionally been forged, machined, welded from dozens of parts. 3D printing, which engineers call additive manufacturing, inverts this. A laser fuses metal powder layer upon layer, building the part up from nothing. There are some real advantages to this approach. An engine printed as one piece sheds the bolts, seals and joints where conventional engines leak and fail; when Skyroot test-fired its Raman engine in 2020, it said the fully printed injector halved the mass and cut components and lead time by 80% against conventional manufacture.

Complex internal plumbing — the fine cooling channels that let Vikram-1’s regeneratively cooled engine chill itself with its own propellant — can be printed in shapes no drill can reach. Prototypes emerge in days, not months, so a startup can test, fail and redesign at a pace that would have been anathema to ISRO’s supplier chains. The downsides are subtler: peer-reviewed surveys of the field flag porosity, rough internal surfaces and batch-to-batch variability, and NASA has documented a printed copper combustion chamber failing on the test stand from degraded material quality. A printed engine, in short, is faster and lighter but demands obsessive quality control — the flaw hides inside the layers.

What is the significance of Vikram’s “all-carbon-composite” body?

If the engine is printed, the airframe is woven. Carbon-fibre composite — filaments of near-pure carbon set in resin — offers specific strength (strength per unit weight) many times that of aerospace aluminium or maraging steel; Skyroot claims a five-fold saving over the best rocket steel. Every kilogram of structure trimmed is a kilogram of satellite gained.

The American company, Rocket Lab’s Electron rocket, pioneered the approach and Vikram-1 follows it. The material also resists fatigue and corrosion and can be laid up by automated machines into seamless tubes — Vikram-1’s Stage-1 is India’s longest single-piece composite rocket stage. The disadvantages: the material and its curing infrastructure are expensive; its strength runs along the fibres, so a poorly designed laminate is strong one way and brittle another; and damage — a delamination from a knock in transport — can lurk invisibly beneath a perfect surface, demanding ultrasonic inspection where a dent in aluminium announces itself.

Is this comparable to ISRO’s PSLV?

In architecture, yes; in scale and philosophy, no. Both are four-stage expendable rockets that end in a restartable liquid stage for precise orbital insertion — Vikram-1’s Orbital Adjustment Module is a miniature cousin of the PSLV’s PS4. Both lean on India’s long mastery of solid propulsion. But the PSLV is a 44-metre, 320-tonne workhorse alternating solid and liquid stages to lift 1,750 kg to polar orbit; Vikram-1 is a 22-metre featherweight stacking three solid stages under its liquid module to carry 350 kg. The PSLV wears maraging steel; Vikram-1 wears carbon.

The nearer ISRO analogue is the SSLV, and there the comparison sharpens. The two are architectural twins: three solid stages capped by a small restartable liquid module, both conceived for small satellites on short notice. On raw capacity ISRO wins: SSLV lifts 500 kg to low earth orbit against Vikram-1’s 350. However Vikram’s all-carbon airframe is leaner than SSLV’s conventional casings, a printed engine line built for faster iteration, and — the deepest difference — institutions. SSLV was designed by the state and its production licensed to Hindustan Aeronautics Limited for ₹511 crore; Vikram-1 is owned outright by its maker, financed by venture capital, priced by the market.