Along the axis of the spacecraft and protruding from the end of the lower cone was an solid propellant injection rocket and rocket case, which formed the main structural member of the spacecraft.
Along the axis of the spacecraft and protruding from the end of the lower cone was an 11 kg solid propellant injection rocket and rocket case, which formed the main structural member of the spacecraft.
Along the axis of the spacecraft and protruding from the end of the lower cone was an 11 kg solid propellant injection rocket and rocket case, which formed the main structural member of the spacecraft.
0.045 seconds.