Are they pushing stuff to geo-synch orbit? Thats where the big business seems to lie. I thought the article was really vague and surprised it did not talk about Space X and other competitors.
Paylod: 110kg
Orbit: 500km, Sun synchronous
Stages: 3
1st stage: 9x "Rutherford"[1] RP/LOX engine
2nd stage: 1x "Rutherford" RP/LOX engine
3rd stage: Solid engine)
Cost: $4.9M
[0] http://www.rocketlabusa.com/[1] http://www.rocketlabusa.com/about-us/propulsion/rutherford/
I hope Rocket Lab will do better. I just asked them for the missing specs like empty and loaded mass of each stage, maximum and minimum ISP of each stage, maximum and minimum thrust of each stage, burn time of each stage, inclination of launch site, payload, inclination, apogaeum and perigaeum of or proposed orbits.