4 Years Of Collaboration And Yet, We Still Work Together.

The Return

It’s been a while since we last lunched a rocket, and funding hasn’t been all that great. But with the Help of SvechLuft and the Creation of the Lavochkin Aerospace will ensure that the space program will keep running.

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..

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.

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...

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]

Another great accomplishment for the mighty Bar! Zodiak, the first SSTO I’ve built.

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.