Actually, OrbitalATK can simply keep using the Atlas V.
Well, other than the fact that AV is getting re-engined as well...
How many are actually available for such use given the need to provide assured access to space for the primary EELV customers?
Yea, I'd think before they signed the contract for the RD-181's is the time to have decided to keep flying on Atlas.
I think there's two separate issues here.
1) Fulfilling NASA's CRS contract.
2) OrbATK becoming a playing in the commercial and USG payload market (as they've said they intended to)
For the first, they may have determined repairing the pad and what are probably fairly minor modifications to mount the RD-181 engines won't be that expensive. The temporary move to Atlas is likely more an issue of time than money. Once Antares is flying again, they won't need Atlas for that, And Antares is likely cheaper for them, and they really only need enough Antares cores and RD-181 pairs to complete the CRS contract. (not sure how many that is).
The second issue becomes more sticky. Antares isn't a great launcher BLEO because of the lack of a high energy upper stage, and most payloads are going BLEO for comsats and USG sats. Wallops is not a good location for those orbits, and Jim has said before that USG won't launch their payloads on an LV that's not launching out of CCAFS for East Coast launches. It also sounds like the pad at Wallops would not be easily modified for vertical payload integration which USG would require.
To compete for USG payloads, OrbATK will also need a West Coast Pad, as I understand. So they'll need a pad at VAFB, or perhaps Kodiak?
And even with a high energy hydrolox upper stage it would probably have performance similar to Atlas V-401. Good for most commercial sats, but I think Antares might need the capability to lift more than that for USG payloads. ULA has the heavier Atlas and Delta variants. SpaceX will have FH. What will OrbATK do? Can they just compete for the smaller payloads or does USAF require they can cover their full payload range? Not sure how that works, but that's a potential issue there. Maybe that means an Antares Heavy, or can the Antares core be adapted to mount ATK GEM-60's? (can they contractually use them for any LV other than Delta?)
So, if I understand correctly, if they really want to compete for USG payloads, OrbATK will need a CCCAFS pad, a West Coast pad, both with vertical payload integration. And perhaps heavier variants to cover the larger USAF/DoD payloads?
I think it's this aspect which really makes relying on the Ukrakian cores in the long run become problematic I think. As well as the Russian engines for reasons ULA is seeing.
A stockpile of cores and the Russian RD-181 contract can get them through the CRS contract flying from Wallops as a short term (and relatively inexpensive) fix for that contract. But beyond that there's a lot of questions with the engine, core, and launch site.
This is where I think boosters using the 3.7m wide composite solids, along with a new hydrolox upper stage could still be in the mix. Wallops couldn't handle that but that would be a moot point as OrbATK would need a CCAFS pad anyway. They can build the new pad to accommodate the large solid motors. And obviously there's rail accommodations to the cape from Utah for such segments. That puts the engines and cores all in-house at OrbATK. As well as upper stage motors that already exist in-house like Castor 120 adn Castor 30XL. Pretty much everything but a new hydrolox upper stage/engines. They’d have options for heavier payloads such as putting three 1st stage motors in a parallel “heavy” configuration, or ringing the single booster motor with GEM-60’s like a Delta II.
And well...ATK has always been fond of such an LV. (Athena III, Liberty)
Regardless of that, I think it has a lot of benefit for OrbATK in the long run. Particularly if SLS survives long enough for NASA to start ordering Advanced solid boosters as they'd use the same casing tooling and propellants.
But this wouldn't be available to quickly get Cygnus launches back in-house to fulfill the CRS contract. They'd be reliant on someone else for several years. So -maybe- the re-engined Antares is more like an interim step using an existing alternate engine on their existing (repaired) pad?