#PRARAMBH

     A NEW
  BEGINNING.
A NEW DAWN.

India's First Private Space Launch


Missionpatch
LAUNCH SUCCESSFUL


VIKRAM-S : MISSION PRARAMBH


The pathbreaking launch mission for the indian private space sector

Prarambh is the mission name of Vikram-S, a single stage suborbital space launch vehicle of Skyroot Aerospace, India’s leading SpaceTech startup and a two-time national award winning space launch vehicle company, with a mission to Open Space for All. Prarambh means the beginning, signifying a new era for the private space sector in India and the first mission for Skyroot. The synergy between Skyroot, ISRO and the Space regulator IN-SPACe forms the bedrock of success for this mission.

With the groundwork starting around late 2020, Vikram-S has been developed within a record time of two years. Vikram-S is powered by the solid-fuelled propulsion, cutting edge avionics and all-carbon fibre core structure.

The Vikram-S will help test and validate majority of the technologies in the Vikram series of orbital class space launch vehicles, including many sub-systems and technologies that will be tested across pre lift-off and post lift-off phases of the launch.


VIKRAM-S : CUSTOMER PAYLOADS

space kidz india

bazoomq armenia

n-space tech india


VIKRAM-S : VITAL STATS

MASS : 545 KG

LENGTH : 6 M

DIAMETER : 0.375 M

PEAK VACUUM THRUST : 7 TONNES

PEAK COMBUSTION PRESSURE : 90 BAR

PEAK VELOCITY CAPABILITY : > MACH 5 [HYPERSONIC]

PAYLOAD CAPACITY : 83 KG TO 100 KM ALTITUDE





VIKRAM-S : THE MODEL



Vikram S

VIKRAM-S : THE SUCCESS SCALE



Vikram Series



VIKRAM-S : QUICK FACTS



ONE OF THE WORLD'S FIRST FEW ALL COMPOSITE SPACE LAUNCH VEHICLES


3D PRINTED SOLID THRUSTERS FOR SPIN STABILITY


TESTS 80% OF TECH FOR FUTURE VIKRAM SERIES OF ORBITAL SPACE VEHICLES


QUICKEST AND MOST AFFORDABLE RIDE TO SPACE


FLIGHT-PROVING OF AVIONICS SYSTEMS IN VIKRAM SERIES LIKE TELEMETRY, TRACKING, GPS, ON BOARD CAMERA, DATA ACQUISITION AND POWER SYSTEMS




VIKRAM-S : MISSION PROFILE



Vikram Series



VIKRAM-S : FLIGHT SEQUENCE*


EVENT TIME, SEC ALTITUDE, KM
IGNITION 0.0 0.0
LAUNCHER LEAVING 0.74 0.01
SPIN MOTOR IGNITION 0.84 0.014
MAX Q 15.59 6.58
BURN-OUT 24.77 17.9
APOGEE 139.93 81.5
SPLASHDOWN 290.97 0.0
*Lower Bound


KALAM 80: STATIC FIRE TEST

SPIN STABILIZATION SYSTEM

Bottom line