Ah, true - forgot about him - but he got explicitly taken out in the same episode.
Tom Paine is also NASA administrator.
Quote from: Blackstar on 03/14/2021 08:42 pmTom Paine is also NASA administrator.Wow, Paine was a real life person?
Yes, surprisingly, there are real people in the space program who are not astronauts.
LOL - I did cite Von Braun & Krantz, who were not astronauts - I'm just saying that the show seems to be defining the character of a real life person like Paine, and casting aspersions on him for dramatic purposes. I feel a little leery about this, because I think that fictional characters can do that stuff without it being at cost of the reputations of real people.
Quote from: ncb1397 on 03/13/2021 06:41 pmQuote from: MATTBLAK on 03/13/2021 07:58 amEven if the payload bay was filled solid with hypergolic propellant tanks; I doubt there'd be enough delta-v and thrust for the OMS engines to slow it into LLO, boost it out of LLO and then slow into LEO. I sincerely doubt the Orbiter shape and TPS could survive a direct-entry into Earth's atmosphere; traveling more than 36,000 feet per second!!Actually, it would be very close to LLO (assuming the dry mass of the orbiter doesn't change much). You could easily fit 300 t of hypergolic fuel in the cargo bay.315*9.8 * ln(370/70) = 5140 m/s.LLO requires almost exactly that (TLI is 3.2 km/s). Of course, 100 t of hydrolox fuel gets you almost the same performance and would also approximately fit in the cargo bay. 453 *9.8*ln(170/70) = 3940 m/s.Hydrolox would require staging in a higher orbit but such a move requires much less propellant mass.Shuttle actually got pretty close to flying a pretty big hydrogen tank in the cargo bay in our timeline through the shuttle centaur program.https://en.wikipedia.org/wiki/Shuttle-CentaurHell, yes. The Shuttle payload bay is a cylinder with a radius of 7.5 feet (15 feet diameter) and 60 feet long. Volume = πr2h= π×7.52×60= 3375π= 10602.9 feet310603 cubic feet are 300 000 L. With a density close from water, 1 L of storable would weight 1 kg, so 300 000 L would be indeed 300 metric tons. Geez, we heard so many times the Shuttle orbiter payload is 30 metric tons, never thought it could carry 10 times that mass in liquid. Crazy, when you think about it. From there, surely, with 300 metric tons of storable props in the bay, it can go... pretty far. TLI or Earth escape takes 3.1 km/s ; LLO takes +1 km/s "in" and +1 km/s "out". How about that... the Shuttle could go to LLO on the freakkin' OMS pods alone. Except the bay would be filled to the brim, so where would the Lunar Module go ? Perhaps send ahead to a lunar orbit space station and the Shuttle crew commute there, to the surface...
Quote from: MATTBLAK on 03/13/2021 07:58 amEven if the payload bay was filled solid with hypergolic propellant tanks; I doubt there'd be enough delta-v and thrust for the OMS engines to slow it into LLO, boost it out of LLO and then slow into LEO. I sincerely doubt the Orbiter shape and TPS could survive a direct-entry into Earth's atmosphere; traveling more than 36,000 feet per second!!Actually, it would be very close to LLO (assuming the dry mass of the orbiter doesn't change much). You could easily fit 300 t of hypergolic fuel in the cargo bay.315*9.8 * ln(370/70) = 5140 m/s.LLO requires almost exactly that (TLI is 3.2 km/s). Of course, 100 t of hydrolox fuel gets you almost the same performance and would also approximately fit in the cargo bay. 453 *9.8*ln(170/70) = 3940 m/s.Hydrolox would require staging in a higher orbit but such a move requires much less propellant mass.Shuttle actually got pretty close to flying a pretty big hydrogen tank in the cargo bay in our timeline through the shuttle centaur program.https://en.wikipedia.org/wiki/Shuttle-Centaur
Even if the payload bay was filled solid with hypergolic propellant tanks; I doubt there'd be enough delta-v and thrust for the OMS engines to slow it into LLO, boost it out of LLO and then slow into LEO. I sincerely doubt the Orbiter shape and TPS could survive a direct-entry into Earth's atmosphere; traveling more than 36,000 feet per second!!
But playing with numbers for split hydrolox/hypergolic for the lunar transport requirements, that may have been the best/most plausible explanation for Season 2s events. The breakdown then is 100 t of hydrolox and 25 t of OMS fuel. The hydrolox provides ~3.2 km/s of delta v for the ~70 t shuttle and the hypergolic fuel does insertion into and out of a high lunar orbit by providng about ~950 m/s of delta V (we know that the LSAM vehicle used for transport up and down from the moon is capable given that it does an in space rendezvous with a CSM on an earth escape trajectory at the end of Season 1). How our shuttle was engineered, the OMS pods already contained over 21 t of fuel so this isn't much of a stretch.
I wonder if the late USSR senile leaders - Brezhnev, Andropov and Chernenko - have gone the same way as Jimmy Carter, that is - were they erased from that timeline ? Brezhnev stagnation and seemingly never ending agony did half of the job of finishing USSR - all by themselves.
In passing, this proves the script writers learned their space history lessons...
So Sally Ride is in the crew of Pathfinder during the following episodes ?
Andropov is the leader of Soviet Union in the latest episode. He is mentioned about Apollo Soyuz which like in our timeline is the final Apollo flight (but much later).I wonder who will win the 1984 presidential election. Schweiker ? Mondale ? Bush ? Dole ?
I found the background history to be fascinating.
Gee, that's a good point - if you have Sea Dragon, why do you even need the Space Shuttle at all? With Sea Dragon, you should even be able to do Mars Direct.(Speaking of which - once they shift toward a Mars storyline, they really need to include at least one scene with Dr Zubrin - that would be priceless )Assuming the Soviets have moved beyond N-1 and are using Energia or something comparably powerful, then they'd be able to put up space stations bigger and better than Mir on their own. Perhaps then there's no need for collaboration on ISS, when each side has such strong lift capabilities of its own.Sadat surviving assassination means Middle East peace has more chance to germinate.Assassination of the Pope means that Soviet hold over Poland stays strong, and Eastern Europe remains firmly under the Iron Curtain.Each of these things helps free up more resources for the superpowers to direct spaceward (which is obviously the intention of the writers.)They keep mentioning Panama for some reason, as a hotspot of contention.