NERO Launches - Rockets to be launched

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NERO $Description: Description: Y:\Webpages\NERO\NERO Running\wwwroot\graphics\pijl.gif$ Launches $Description: Description: Y:\Webpages\NERO\NERO Running\wwwroot\graphics\pijl.gif$ Rockets to be launched

Rockets and/ore static rocket engines tests

On this page there will be information and planning about :

- rockets to be launched

- static rocket motors to be tested.

ROCKET LAUNCHES

Rocket details

Status of details: FINAL

	Simplicio	*TinTin*
club	Studenten D. Verhaeghe VRO-VTI Torhout	Studenten D. Verhaeghe VRO-VTI Torhout
country	Belgium	Belgium
length, (m)	1,910	1,910
diameter, (mm)	78	78
mass lift-off, (kg)	7,12	7,12
maximum speed, (m/s)	153	153
altitude, 85° elev. (m)	1160	1160
range, 85° elev. (m)	TBD	TBD
range, 75° elev. (m)	TBD	TBD
flight time to top of trajectory, (s)	16	16
total flight time, (s)	126	126
motor type/propellant	Cesaroni Pro54 3 grain reload kit 1261-J449-15A Blue Streak, AP/PVC	Cesaroni Pro54 3 grain reload kit 1261-J449-15A Blue Streak, AP/PVC
propellant mass (kg)	0,624	0,624
total impulse (Ns)	1260	1260
burning time (s)	2,8	2,8
parachute type be aware ! the descending time by parachute from top of trajectory to touchdown is maximum 120 sec.	singel stage: - lateral servo-hatch	singel stage: - lateral servo-hatch
means of recovery	acoustic beacon yellow body with red fins	acoustic beacon yellow body with red fins
instrumentation	RDAS Tiny (recovery) - servo system - pressure - acceleration	RDAS Tiny (recovery) - servo system - pressure - acceleration - video camera

TBD = to be determined

TBC = to be confirmed

STATIC ROCKET ENGINE TESTS

Leo dB

- concentric hybrid rocket engine

Jan V. two N2O/MeOH rocket engine

- NITROUS ? (N2O/Kero motoren)

- NITROUS ? (N2O/Kero motoren)