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Launch vehicle design updates—VAJRA and PADMA configurations, specifications, and program milestones.

VAJRA — Reusable Micro-Launch Vehicle Design

VAJRA — Reusable Micro-Launch Vehicle Design

Program update · 2025

Gatkul’s VAJRA is a two-stage, fully reusable launch vehicle engineered for frequent smallsat missions to Low Earth Orbit—combining RAGAM MethaLOX boost with a vacuum HydroLOX upper stage and regenerative reentry cooling.

  • • Payload: up to 500 kg to LEO
  • • Stages: 2 (both reusable)
  • • Stage 1: RAGAM MethaLOX, vertical RTLS
  • • Stage 2: HydroLOX, regenerative heat shield
PADMA — 30-Ton Class Human-Rated Launcher Design

PADMA — 30-Ton Class Human-Rated Launcher Design

Program update · 2025

PADMA (Precision Advanced Deep-space Mission Architecture) is a three-stage, human-rated architecture for LEO infrastructure, crew transport, and Earth–Moon logistics—with a dual-use Stage 2 designed for orbital station modules after ascent.

  • • Payload: up to 30 t to LEO
  • • Stages: 3 (Stage 1 & 3 reusable)
  • • Engines: RAGAM + vacuum HydroLOX
  • • Human-rated avionics; lunar logistics ready
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