HiakaSat

 2015-F03

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ORS-4 / Hiaka - 55 kg 38.8"dia 10" tall wafer adapter, intended to track volcanic activity in HI chain; HIAKA = Hyperspectral Imaging Aeronautical Kinemtic Analysis. Also, AFSS (Autonomous Flight Safety System) as second payload.

Super Strypi used a modified VAFB SLC5 Scout rail launcher built at WSMR and installed at to Kauai / Kokole Point. The rocket is spin-stabilized and uses three Aerojet solids, LEO-46, LEO-7 and LEO-1.

The vehicle spun out of control in the latter part of the first stage burn and the mission was aborted.

ORS-4
Date	Time	Event	Orbit
2015 Nov 4	0345	Launch by Super Strypi	Kauai LC41
		T+0:55? Vehicle failed, 30 km?
		Impact Pacific

ORS-4 plan
Date	Time	Event	Orbit
		T+1:22 St 1 cutoff 69 km
		T+1:38 St 1 sep 94 km
		Despin? T+1:42
		T+1:56 Fairing sep 118 km 20.6N 159.9W	-6105 x 208
		T+3:00 St 2 burn 178 km 19.3N 148W	-6000 x 210
		T+4:02 St 2 burnout 17.5N 160.3W 243 km 5.132 km/s	-4762 x 454
		T+4:48 St 2 sep 306 km 15.5N 160.5W 5.02 km/s	-4761 x 453
		T+6:46 St 3 burn 417 km 10.74N 161.10W 4.827 km/s	-4759 x 453
		T+7:32 Perigee positive, 430 km 8.4N 161.4W 7.6km/s	20 x 430
		T+7:40 St 3 burnout 7.90N 161.52W 430 km	430 x 496
		T+9:47 Hiakasat sep
		T+10:52 Cubesat deploys, 4 small
		T+10:54 Cubesat deploys, 4 small?
		T+10:59 Cubesat deploys, 3 mixed
		T+11:01 Cubesat deploys, last one (6U?)
		T+11:47 RCS depletion

Payload:

• Hyperspectral imager