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Finally back with some updates.
Getting a multistage platform to launch for a Spacecraft3 vessel has kicked my behind, but it's finally getting closer. Hopefully within the week there will be a beta up on the Hanger for people to take for a spin. Much thanks to Liber and Sputnik for assistance with this.
Meanwhile I've been rethinking and recalculating things. I thought I'd offer up a bit of the background context that this project is coming out of, as I've been spending even more time writing lately than I have been working on this project. Honestly, I love how I can try out ideas with Orbiter and then use what I learn to re-inform what I'm working
on.
ZanTar-Cheetah's Daedalus B-52 catamaran and the Icarus manned micro-shuttle (refurbished-remodeled Boeing X-37Bs) happen in the Spring of 2022 and herald the next wave of SpaceX. The B-52s were purchased from a boneyard outside of Tuscan, Arizona and totally renovated utilizing both titanium alloys and carbon-composites. ZanTar-Cheetah (who go on to create the first cislunar tether-sling transportation network over the next decade - which also ties into their name) was founded by a group of dot-commers who came out of the last financial crises mostly unscathed which might help to explain the "bold" choices of both co. logo and design elements.
The latest changes to the Daedalus and Icarus:
Daedalus power plants - primary: 4 X GEnx-2B67 (recycled and refurbished from 747s), 66,500 lfb (296 kN) = 1184 kN
Secondary - 8 × Pratt & Whitney TF33-P-3/103 turbofans, 17,000 lbf (76 kN) = 608 kN
The 2 inner GEnx engines are spooled down for launching the Icarus platform, and the 8 Pratt & Whitney's are turned on then to compensate. Note this would result in a net gain of 16 kN thrust for pitching up for launch attitude. Naturally this can't be replicated with Spacecraft3, but I have tried to reflect these things in the model. It's the reason that I've disabled all the engine exhaust except for the GEnx's.
The Daedalus really can't be flown without it's rocket payload safely above about 40% full throttle. It wants to go supersonic.
The Icarus launch platform consists of 2 Castor 120s as stages, with 3 Castor 4B boosters attached to the first stage. The total weight of the Icarus and rockets is about 140982 kg, which is why ZTC was forced to revamp the catamaran using so many composites. The original B-52 was designed to carry about 1/5 this weight. Still, I have great confidence in the ZTC engineers.
The latest revision of the ZTC-Daedalus B-52 catamaran test flight out of Rochambeau.
Rochambeau test flight with Icarus launch platform attached. The Daedalus requires trim with the payload.
Multistage2 experimental flight. Note the relatively small size of the platform. I've been unable to achieve orbit test launching from the ground like this. However, aerial launches from between 50 and 60 thousand feet have been successful (15.24 - 18.29 km).
Getting a multistage platform to launch for a Spacecraft3 vessel has kicked my behind, but it's finally getting closer. Hopefully within the week there will be a beta up on the Hanger for people to take for a spin. Much thanks to Liber and Sputnik for assistance with this.
Meanwhile I've been rethinking and recalculating things. I thought I'd offer up a bit of the background context that this project is coming out of, as I've been spending even more time writing lately than I have been working on this project. Honestly, I love how I can try out ideas with Orbiter and then use what I learn to re-inform what I'm working
on.
ZanTar-Cheetah's Daedalus B-52 catamaran and the Icarus manned micro-shuttle (refurbished-remodeled Boeing X-37Bs) happen in the Spring of 2022 and herald the next wave of SpaceX. The B-52s were purchased from a boneyard outside of Tuscan, Arizona and totally renovated utilizing both titanium alloys and carbon-composites. ZanTar-Cheetah (who go on to create the first cislunar tether-sling transportation network over the next decade - which also ties into their name) was founded by a group of dot-commers who came out of the last financial crises mostly unscathed which might help to explain the "bold" choices of both co. logo and design elements.
The latest changes to the Daedalus and Icarus:
Daedalus power plants - primary: 4 X GEnx-2B67 (recycled and refurbished from 747s), 66,500 lfb (296 kN) = 1184 kN
Secondary - 8 × Pratt & Whitney TF33-P-3/103 turbofans, 17,000 lbf (76 kN) = 608 kN
The 2 inner GEnx engines are spooled down for launching the Icarus platform, and the 8 Pratt & Whitney's are turned on then to compensate. Note this would result in a net gain of 16 kN thrust for pitching up for launch attitude. Naturally this can't be replicated with Spacecraft3, but I have tried to reflect these things in the model. It's the reason that I've disabled all the engine exhaust except for the GEnx's.
The Daedalus really can't be flown without it's rocket payload safely above about 40% full throttle. It wants to go supersonic.
The Icarus launch platform consists of 2 Castor 120s as stages, with 3 Castor 4B boosters attached to the first stage. The total weight of the Icarus and rockets is about 140982 kg, which is why ZTC was forced to revamp the catamaran using so many composites. The original B-52 was designed to carry about 1/5 this weight. Still, I have great confidence in the ZTC engineers.
The latest revision of the ZTC-Daedalus B-52 catamaran test flight out of Rochambeau.
Rochambeau test flight with Icarus launch platform attached. The Daedalus requires trim with the payload.
Multistage2 experimental flight. Note the relatively small size of the platform. I've been unable to achieve orbit test launching from the ground like this. However, aerial launches from between 50 and 60 thousand feet have been successful (15.24 - 18.29 km).