Lav 44
Heres some new aircrafts that might make it into the market by next week.
Lav 44
Cost: 107,494 Mass: 35,433kg LiquidFuel: 11,000kg Parts: 52 Passengers: 64
Lotus 700-A
Cost: 184,482 Mass: 80,400kg LiquidFuel: 13,600kg Parts: 123 Passengers: 80
SL 407
Cost: 131,962 Mass: 55,608kg LiquidFuel: 21,200kg Parts: 93 Passengers: 96
Do note that they might change over time...
More Posts from Zvedagrad and Others
Icarus: So taking Kazakh’s YouTube channel wasn’t as easy as I thought it was, yet again, nothing ever that easy. Doesn’t simply matter, as I said, that channel will still change whether like it or not.
Sorry Kaz, nothing personal...
(via https://www.youtube.com/watch?v=m-B05fXqe74)
The SL-400 Zori made it’s first successful air-launch by sending a small GPS satellite into LKO...
More air-launchers will be scheduled soon.
A Concept Design
So I was helping out the bureau team from the EASA and Despite there knowledge they did come out with some interesting concept designs. And what was suppose to be a space shuttle it became into a this, a forward sweep wing design. But regardless, it is a concept design, and I have no intention on creating a super sonic jet...
[SvechLuft]
The Hrot Rocket Family
Last night, our crew ended up testing an old rocket design. Using only the RE-M3 Mainsail and 8 of 24-77 Twitch engines on the first stage. And the second stage having 4 LV-T95 Swivel.
Grot-1
Delta-V:2,639 / 5,143 m/s
Mass: 79,098 / 105,100 kg
TWR: 1.46
Parts: 44
LiquidFule: 36,000 kg
Oxidizer: 44,000 kg
SolidFule: 48 kg
MonoProp: 220 kg
Hrot-2
Delta-V: 1,552 / 5,606 m/s
Mass: 82,245 / 152,638 kg
TWR: 1.79
Parts: 58
LiquidFule: 36,000 kg
Oxidizer: 44,000 kg
SolidFule: 39,060 kg
MonoProp: 220 kg
Hrot-3
Delta-V: 1,944 / 5,843 m/s
Mass: 134,439 / 201,174 kg
TWR: 1.90
Parts: 72
LiquidFule: 36,000 kg
Oxidizer: 44,000 kg
SolidFule: 78,072 kg
MonoProp: 220 kg
Hrot-4
Delta-V: 3,568 / 6,345 m/s
Mass: 221,698 / 266,298
TWR: 1.58
Parts: 71
LiquidFule: 95,400 kg
Oxidizer: 116,600 kg
SolidFule: 96 kg
MonoProp: 220 kg
More extensive testing on the Soyuz T-3CR, it isn't the most ideal thing to have such powerful engines, however changing it’s flight curvature might be efficient and safer for both the payload and rocket with out having to stress the tanks during flight.
Back online, hopfully. Although I do remember saying on Twitter that im gonna give a little more information in tumbler on certain events that happens in the EFSA. however im not be the best writer, but I’ll do my best regardless.
So not much has been happening here on Tumbler, although more Activity has been going on over in Twitter and I do apologies with the lack of content. But I will try to do at least something, perhaps more details on projects, missions, ect..
