Distributed launch of Noble gasses SEP propellant for Noble gas pressurized habitats
Come back later today or tomorrow for the results or read our previous posts on dual use habitats as SEP propellant tanks and as habitats. Might require distributed launch of breathable atmosphere.Look up ULA’s Distributed launch.
SpaceX Dragon auto gyrating helicopter as planetary descent probe
would this work for planetary atmosphere probes and/or soft landers?
Kickstarter campaign to raise funds to hire a SBIR grant writer
(A)(1) Hire the SBIR professional writer you propose to hire for that SBIR proposal to write with you the Kickstarter campaign.
(A)(2) Design the kickstarter to account for phases of research not funded by SBIR or to perform low cost research before SBIR win.
(A)(3) write design the Kickstarter campaign to account for Phase I SBIR loss but set up the possibility to perform research on a Phase II SBIR.This means the Kickstarter might be able to fund Phase I with appropriate rewards to donors
(B)(1) A related idea that can be used in conjunction with the Kickstarter campaign to raise funds to hire a SBIR grant writer would be this earlier post; https://yellowdragonblog.com/2015/06/15/intern-to-subcontractor-mentor-protege-a-model-program/
(C)(1) Use Kickstarter IndieGoGo funds to transfer to NASA space act agreement NASA center work on behalf of our terrestrial & cislunar exploration technologies start up.
Best use of our propellant tank ring atomizer/diffuser
Launch from Earth is best served with dense fuel so a heavy launch vehicle might be best served with Propane propellent CBC’s that feed into a Methane core stage using our proposed ring atomizer/diffuser in the core stage with crossfeeding.
The propane should form a slush in the cryogenic Methane or alkenes gelled in alkanes for our proposed dial a propellant with a gravity feed ring atomizer at the bottom of the core stage.
This would be a three core heavy launch vehicle with a cluster of 8 to 10 BE-3 in the core stage and two CBC with two each LNG pBE-4’s.The Blue Origin core stage would appear remarkably similar to the SpaceX heavy core stage.
Crossfeed The LNG into a ring atomizer in the bottom of the LH2 Tank to gell it.The alternative is to have two Vulcan CBC’s on the existing Delta-IV and modify the RS-68 to take a gelled propellant for a minute and a half of flight.
“Rappolee flowers”; payload fairing deployed arbitrarily large structures
(A)(1)Large payload fairings are the backbone of deployed SIGINT, ELINT, radio telescope, and powersats.(NRO and NSA customers)
(A)(2)
http://planet4589.org/nro/nro.html
This idea is from my 2009 lab notebook along with utilizing two docked Dragons as aerodynamic decelerators.Will add to this post over time…….
payload fairing/shroud as upper stage deorbiting mechanisms…..
CONOPS; The Galileo Jupiter probe failed communications antenna had a mesh antenna so our payload fairing could deploy a mesh antenna or solar arrays or SIGINT/ELINT eavesdropping antenna hundreds of M3
Second post here;
New post for 2022 below
Rappolee flowers 2.0 payload fairing solar voltaic for wetlabs (Falcon second stage)
We propose to utilize a CubeSat with a space-based microscope to examine defrosted mice gametes, Zygotes,2 cell,4 cell,8 cell, Compact Morula, example early blastocyst.
These 8 specimen types would be in a cryogenic Nitrogen and would require a mechanism to retrieve small samples and defrost.each sample would require observation at timed intervals and each sample type would act as a control for the example
would be gametes
proposed CubeSat names
Zygote/Sat
Uni/sat
Mouse/Sat
Xenon/Ullage/Sat
Neon/pressurent/sat
A protocol for brewers spent grains and a noodle manufacturer for local tastes
A first example I derive from Soba noodles much loved in Japan and elsewhere.
And a most excellent program NHK Japanology “SOBA”
To use a spent brewer’s Buckwheat we need to find evidence of brewers who use buckwheat, youtube has sparse evidence of this, however, buckwheat and others are being used to brew gluten-free drinks.The second idea is to dry the spent Buckwheat utilizing smoke from a meat smoking operation.This, in turn, would give any spent grain made into flour a smoky essence and make its way into the noodles. Spent grain can be made into bread https://piewithsparkles.wordpress.com/tag/spent-grain/
The American rust belt could also have 1,500 small noodle making export mini business with our richness in grains and soybeans
Skylab-II Max utilizes the maximum payload capability of SLS or BFR to LEO, This should be larger than the proposed Skylab-II.The Skylab-II is pressurized with air or Xenon.(A)(1) inside the spacecraft and all around the outer wall are bottles/tanks of compressed Xenon.This needs study has a radiation shield. ARRM derived SEP tug docks with Skylab-II Max.SEP tug is 10 Tons of Xenon, we need to study the weight of Xenon and air on the Skylab-II.Study mission design of this system to cislunar from LEO and Mars DRM.Skylab-II Max would loft an LH2 tank with all 5 barrels and end caps.Skylab-II MAX is essentially lofting into LEO a SLS first stage as a payload
(A)(2)prepositioning any habitat before crew arrival with the habitat serving as SEP propellant tank should greatly extend any mission design.
Yellow Dragon, a mission to repurpose existing ideas into new ideas 