Using a SpaceX rocket as a cheap(er) launch platform
https://warontherocks.com/2020/06/w...les-dont-copy-russia-and-china-leapfrog-them/
https://warontherocks.com/2020/06/w...les-dont-copy-russia-and-china-leapfrog-them/
Given the frequently quoted 6km/second, how many tungsten dart equivalents to a Tallboy could a Falcon Heavy or BFR put into a polar orbit?
There seems to be little point in going for tactical nuke yields
Simple math. What is the mass of each "dart?" What is the payload capability of the launch system? Knock off some good percentage of the total paylaod to serve as the buss and de-orbit system, and there ya go.
Starship is supposed to have a payload of 100 tons to LEO, at *about* 7.8 km/sec for a kinetic energy of the payload being ~3E12 Joules... or about 0.727 kilotons. That's for the *entire* payload. Cut the mass in hald for bus/de-orbit, and you're down to 0.36 ktons. Split it, say, ten ways, and you're down to 0.036 ktons per weapon. Shave off some drag losses, and you're perhaps 0.02-0.03 ktons per. From 4.6 kilotons of explosive power on the pad, you're down to less than one percent of that per weapon for ten weapons.
Energy efficiency factors into a weapons usefulness, but it's a small consideration. The attractiveness of the tungsten dart concept (Rods from God) is its ability to deliver devastating force quickly, anywhere on the globe, for which there is no known effective defense (except burying the target deeper). Delivering the same force via a more efficient, slower, more vulnerable mechanism is an inferior solution if it doesn't get the job done, even if it is, according to an energy budget, more efficient.Given the frequently quoted 6km/second, how many tungsten dart equivalents to a Tallboy could a Falcon Heavy or BFR put into a polar orbit?
Simple math. What is the mass of each "dart?" What is the payload capability of the launch system? Knock off some good percentage of the total payload to serve as the bus and de-orbit system, and there ya go.
There seems to be little point in going for tactical nuke yields
Little possibility of it, either. Total "yield" of the kinetic weapons is substantially less than the total yield of the chemical propellants in the booster required to orbit them, and few boosters have enough propellant to be classed in the tactical yield capability, unless you're talking about pathetically small yield devices like Davy Crockett. Starship/Super Heavy has 3.4 kilotons of propellant in the first stage, 1.2 kilotons in the second, total of 4.6 kilotons. Some sizable fraction of that is simply tossed away due to gravity and aerodynamic losses. More lost due the mass of the buss and de-orbit systems. More due to drag losses to the weapons.
Starship is supposed to have a payload of 100 tons to LEO, at *about* 7.8 km/sec for a kinetic energy of the payload being ~3E12 Joules... or about 0.727 kilotons. That's for the *entire* payload. Cut the mass in half for bus/de-orbit, and you're down to 0.36 ktons. Split it, say, ten ways, and you're down to 0.036 ktons per weapon. Shave off some drag losses, and you're perhaps 0.02-0.03 ktons per. From 4.6 kilotons of explosive power on the pad, you're down to less than one percent of that per weapon for ten weapons.
You can do better by making the Starship stage fully expendable, but you're still tinkering with tiny percentages.
Depends how you construct the carrier satellite, you could build it up like a space station over time.Given the frequently quoted 6km/second, how many tungsten dart equivalents to a Tallboy could a Falcon Heavy or BFR put into a polar orbit?
Energy efficiency factors into a weapons usefulness, but it's a small consideration.
Depends how you construct the carrier satellite, you could build it up like a space station over time.
Energy efficiency factors into a weapons usefulness, but it's a small consideration.
Irrelevant to the point at hand, which was to debunk the oft-claimed power of Thor being equivalent to a "tactical nuke." A 5.56mm bullet is also nothing like a nuke, but pointing that out doesn't imply that the bullet isn't militarily useful.
You mean like Brilliant Pebbles plus Brilliant Rods?Or alternatively, you could construct a relatively lose satellite constellation with a command platform at its heart and some defensive ASAT/Anti-Missile weapons scattered around the outer edges.
You mean like Brilliant Pebbles plus Brilliant Rods?
Talking about the maximum speed reached for a "rod of god", here some details:
For attacking hardened or deeply buried targets, the long rods would not outperform existing missiles equipped with conventional penetrating warheads. That's because the physics of high velocity impacts limits the penetration depth; basically, too much energy at impact causes the projectile to distribute its energy laterally rather than vertically. Tests done since the 1960s by Sandia National Laboratories, in Albuquerque, N.M., confirm that for even the hardest rod materials, maximum penetration is achieved at a velocity of about 1 to 1.5 km/s.
Above that speed, the rod tip liquefies, and penetration depth becomes essentially independent of impact speed. Therefore, for maximum penetration, the long rods would need to be slowed to about 1 km/s, thereby delivering only one-ninth the destructive energy per gram of a conventional explosive-or about 1.5 percent of the potential energy the rod had in LEO. The wasted energy would be immense, and the effort, cost, and complexity of such an orbital system would be entirely out of proportion to the results.
What is DPU?
Depleted Uranium
Elon better get to workThey're reiterating that bullcrap claim again.
A Rod from low orbit is unlikely to hit at anything exceeding orbital speed, 7.8 km/s, unless it has been fired from a giant railgun. More probable speeds are 1-4 km/s.
An object at 3 km/s packs KE equivalent to its mass in TNT. An object at 7.8 km/s has KE around 6.8 times it mass.
If you want a kiloton impact, you need a 150-tonne Rod.
Now he's promising a hour turn aroundElon better get to workThey're reiterating that bullcrap claim again.
A Rod from low orbit is unlikely to hit at anything exceeding orbital speed, 7.8 km/s, unless it has been fired from a giant railgun. More probable speeds are 1-4 km/s.
An object at 3 km/s packs KE equivalent to its mass in TNT. An object at 7.8 km/s has KE around 6.8 times it mass.
If you want a kiloton impact, you need a 150-tonne Rod.![]()
Yeah, it's not clear how much we should read into this. A government official tweeting a link to something as stupid as this is a bit unsettling. It implies that this guy doesn't know diddly squat. In fact, the discussion about "prompt global strike" happened a decade ago, and it's about very different methods. So simply by tweeting that, this guy implies that he's clueless.They're reiterating that bullcrap claim again.
What if it's been accelerated downwards by a rocket motor?They're reiterating that bullcrap claim again.
A Rod from low orbit is unlikely to hit at anything exceeding orbital speed, 7.8 km/s, unless it has been fired from a giant railgun. More probable speeds are 1-4 km/s.
An object at 3 km/s packs KE equivalent to its mass in TNT. An object at 7.8 km/s has KE around 6.8 times it mass.
If you want a kiloton impact, you need a 150-tonne Rod.
I hope you're not just finding out politicians know diddly squat about most things.Yeah, it's not clear how much we should read into this. A government official tweeting a link to something as stupid as this is a bit unsettling. It implies that this guy doesn't know diddly squat. In fact, the discussion about "prompt global strike" happened a decade ago, and it's about very different methods. So simply by tweeting that, this guy implies that he's clueless.They're reiterating that bullcrap claim again.
What if it's been accelerated downwards by a rocket motor?
What if it's been accelerated downwards by a rocket motor?They're reiterating that bullcrap claim again.
A Rod from low orbit is unlikely to hit at anything exceeding orbital speed, 7.8 km/s, unless it has been fired from a giant railgun. More probable speeds are 1-4 km/s.
An object at 3 km/s packs KE equivalent to its mass in TNT. An object at 7.8 km/s has KE around 6.8 times it mass.
If you want a kiloton impact, you need a 150-tonne Rod.
mmm, as with sand castles, you just need to let the tide come in. Some weapons could assist with that, probably without needing to go into space, and come back, first.What if it's been accelerated downwards by a rocket motor?
Possible, but the cost of launching the suitable rocket motor into orbit...
Orbital kinetic strikes are good weapon even without that; they are perfect choice against such targets, as, say, Chinese island fortresses.
mmm, as with sand castles, you just need to let the tide come in. Some weapons could assist with that, probably without needing to go into space, and come back, first.
What if it's been accelerated downwards by a rocket motor?
There's no point to actually put it in orbit these days. Assuming you actually hit the target these days, which is completely possible given PGMs not as much energy is needed. I guess it's a matter of how many submunitions this concept can fit to make it worthwhile.What if it's been accelerated downwards by a rocket motor?
Once more, with feeling: If you have a kinetic weapon, unless you play some terribly complex games with gravity by slinging it from planet to planet in a complex decade-long dance, you only get *out* of the weapon what you put *into* it.
Think of a bullet: how destructive is it? To first order, how much gunpowder was used tells you how destructive it is. Those fifty grains of gunpowder are the *maximum* total energy that can be packed into the bullet. So with a Rod From God, the total energy of the weapon will come from the rockets that boosted it. If you pile all the rockets used, from the multi-stage space launch system to the orbital maneuvering system to the de-orbit booster, do you have a nuclear weapons worth of energy? No, you don't, unless your weapon was hefted by a Sea Dragon.
I dont see this weapon as being used as a mass attack, mainly because of the scale of the earth v the costs, of launch mainly.
Rather see it as an ability to deliver a 'hellfire' anywhere, within minutes, in support of a SF team, or an agent in trouble. So a few hundred missiles should cover much of the occupied earth.
That's probably why G2G with LEO maneuvering is better.I dont see this weapon as being used as a mass attack, mainly because of the scale of the earth v the costs, of launch mainly.
Rather see it as an ability to deliver a 'hellfire' anywhere, within minutes, in support of a SF team, or an agent in trouble. So a few hundred missiles should cover much of the occupied earth.
Orbital mechanics don't help with this. It's going to take at least a few tens of minutes between starting a deorbit burn and actually hitting atmosphere And then there's a question of how long it takes to get an object to the right place in its orbit to begin that deorbit burn and actually hit the aimpoint you want. Without aerodynamic maneuvering (aka braking) you really don't get much cross-range adjustment here. So you need a lot of objects in a LOT of different orbits to have one available to deorbit onto a specific aimpoint on really short notice.