NationStates Jolt Archive

UNDER CONSTRUCTION

Nolan-Petyav Aerospace Propulsion Industries
This storefront is considered modern tech, upto 2020. All items below are copyright Nolan-Petyav Industries. Any infringement will result in full use of legal actions, as well as possible military action.

NP-21E Turbojet (http://www.aeroworldnet.com/images/fth15.jpg)
Dry Weight: 2273kgs
Length: 4.88442m
Width: 1.2319
Thrust Developed: 14,515kg's at Sea Level
Nozzle Arrangement: 3D Thrust Vectored; Vertical: -25*, +25; Horizontal: -12*, +35;
Description: A great engine for single powerplant aircraft, extremely reliable, so stalls are not an issue. The Three-Dimensional Thrust Vectoring provides an insane amount of agility to any aircraft, add the incredibly speed from this engine and you have a very intimdating fighting machine. If used in a dual role, the nozzels can only turn in on a 12* angle to prevent damage to the aircraft.
Price: $650,000; Production Rights: $42,000,000

NP-126F Turbojet (http://www.aeronautics.ru/img/img006/al-41f_001.jpg)
Dry Weight: 2688kgs
Length: 5.332m
Width: 1.48m
Thrust Developed: 17,288kg's at Sea Level
Nozzle Arrangement: 2D Thrust Vectored; Vertical: -25*, +25;
Description: The basic tandem engine design from Nolan-Petyav Industries; This engine is also incredibly reliable, like most engines from this company. It provides an incredible amount of thrust, propelling any aircraft over mach 1. Slightly longer and wider than the NP-21E, this engine is designed for larger aircraft, such as the Su-27 series or F-15.
Price: $984,000; Production Rights: $68,000,000

NP-130G Turbojet (http://www.airforce-technology.com/contractor_images/pratt_whitney/3_FCD500_1_low.jpg)
Dry Weight: 2854kgs
Length: 5.982m
Width: 1.51m
Thrust Developed: 21,918kg's at Sea Level
Nozzle Arrangement: 3D Thrust Vectored; Vertical: -25*, +25; Horizontal: -12*, +35;
Description: This engine much resembles the NP-126F, in reliablity and purpose. However, this engine is significantly more powerful, and features full thrust vectoring. This engine is the last "conventionally powered" system provided by Nolan-Petyav Industries.
Price: $1,021,000; Production Rights: $81,500,000

NP-131H Pulse Detonation Engine (PDE) (http://www.isas.ac.jp/e/snews/2001/image/12_04.jpg)

http://phoenixnavigation.com/images/tech/ttuavgas.jpg

Dry Weight: 3120kgs
Length: 5.182m
Width: 1.623m
Thrust Developed: 66,597kgs at Sea level
Nozzle Arrangement: 2D Thrust Vectored; Vertical: -25*, +25; However, must be at 0* for Pulse Det
Description: This is a culmination of years and years of research. This propulsion system features Pulse Detonation which detonates the air/fuel mixture rather than just allowing it to simply deflagrate (burn vigorously). Once a fresh air-fuel charge has been drawn into the pipe, a much smaller amount of a very volatile fuel (such as hydrogen) and an oxidizer (such as oxygen) are injected into a trigger chamber at the closed end of the pipe. This mixture is then ignited by an intensely powerful electrical discharge and made to detonate by forcing it through some carefully designed passages which create high levels of turbulence in the burning mixture. Nolan-Petyav offer a special sleeve that will absorb the tremendious vibrations, so as not to damage the airframe itself. Nolan-Petyav Industries recommends you use this engine in larger aircraft such as a high-alt bomber or reccy aircraft.
Price: $2,570,000; Production Rights: $550,000,000

NP-999-QNF Hafnium (http://www.eurofighter.starstreak.net/Eurofighter/images/3dtvc-action3.jpg)
http://www.eurofighter.starstreak.net/Eurofighter/images/3dtvc-3d.gif
Dry Weight: 5,250kgs
Length: 6.064m
Width: 1.348m
Thrust Developed: 75,812kgs at Sea Level
Nozzle Arrangement: 3D Thrust Vectored; Vertical: -40*, +40*; Horizontal: -12*, +40;
Description: This is also a revolutionary engine, and incredibly powerful. This engine uses Hafnium to create thrust. This obtains energy by using X-rays to encourage particles in the nuclei of radioactive hafnium-178 to jump down several energy levels, liberating energy in the form of gamma rays. Used in a UAV at low speeds, it could extend its range to several months. However fighter aircraft would use it at such a high rate, it would last them about 6 hours at full burn. Of course on most fighter jets this would mean a trip around the world and back. The structural composition of hafnium hinders the release of this radiation, and once the X-Ray is turned off, the Radiation levels severely plummit, meaning if knocked down, there would be no danger.
Price: $1,750,000; Production Rights: $605,000,000

NP-1707-QNF Hafnium Propellant (http://www.arnold.af.mil/aedc/highmach/images/0029025.jpg)
Dry Weight: 8,5490kgs
Length: 7.141m
Width: 1.948m
Thrust Developed: 88,812kgs at Sea Level
Nozzle Arrangement: 2D Thrust Vectored; Vertical: -40*, +40*;
Description: The NP-1707-QNF is a heavy version of the NP-999-QNF engine. It is designed for transport or strategic bomber aviation, and provides an incredible 89,000kg's of thrust. The engine features a larger amount of Hafnium, giving bombers a greater strike distance and more loiter time over a target if necessary.
Price: $1,890,000; Production Rights: $650,000,000

Missile Propulsion

NP-M-62 Rocket
Dry Weight: 150kg's
Length: 0.886m
Width: 0.250m
Thrust Development: 6800kg's at sea level
Nozzle Arrangement: Standard
Description: Standard rocket engine, perfect for Land attack missiles, and maybe ASM's. The 5100kgs of thrust should propell any missile to around mach 3.5, 4 if its light.

NP-M-63 Rocket
Dry Weight: 180kgs
Length: 0.925m
Width: 0.255m
Thrust Development: 8,000kg's at sea level
Nozzle Arrangement: 3D thrust vectoring; 30*
Description: Second generation of rocket engine, same use as above, but more capable due to thrust vectoring. 8,000kgs of thrust can propell missile to mach 4 to mach 4.5.

NP-M-64 SCRAMjet
Dry Weight: 200kgs
Length: 1.045m
Width: 0.423m
Thrust Development: 10,210kgs at sea level
Nozzle Arrangement: 3D thrust vectoring; 45*
Description: Land Attack and ASM engine; Speed of Mach 5 to Mach 6; very long range and full thrust vectoring.

NP-M-71 Rocket
Dry Weight: 75kgs
Length: 25cms
Width: 12.5cms
Thrust Development: 2,300kg's at sea level
Nozzle Arrangement: 3D thrust vectoring; 45*
Description: Perfect engine for an ATGM, highly maneuverable with 45* of thrust vectoring. 2,300kg's will allow for Mach 2 to 3 speed for an ATGM.

NP-M-80 Rocket
Dry Weight: 105kgs
Length: 38cm's
Width: 15.5cm's
Thrust Development: 3,600kg's
Nozzle Arrangement: 3D thrust vectoring; 45*
Description: Rocket motor for a short range AAM; Mach 3 or 4 depending on weight of missile.

NP-M-81
Dry Weight: 115kgs
Length: 44cm's
Width: 17cm's
Thrust Development: 3,950kg's
Nozzle Arrangement: 3D thrust vectoring; 45*
Description: Ideal for a medium range AAM; Mach 3 or 4, but longer range.

NP-M-83
Dry Weight: 120kgs
Length: 50cm's
Width: 17cm's
Thrust Development: 4,200kgs
Nozzle Arrangement: 3D thrust vectoring; 45*
Description: Ideal for Long range AAM; Mach 3 or 4, range of about 200kms for most missiles.

NP-M-91 SCRAMjet
Dry Weight: 200kgs
Length: 65cm's
Width: 20cm's
Thrust Development: 3,400kg's
Nozzle Arrangement: 3D thrust vectoring; 45*
Description: Designed for a short-ranged AAM; This engine would give the missile a speed of mach 4 to 5, with a range anywhere between 50 and 75 miles.

NP-M-92 SCRAMjet
Dry Weight: 250kgs
Length: 73cm's
Width: 25cm's
Thrust Development: 4,120kg's
Nozzle Arrangement: 3D thrust vectoring; 45*
Description: Medium Range AAM; Mach 4 to 5, range of 100 to 150 miles.

NP-M-93 SCRAMjet
Dry Weight: 275kgs
Length: 80cm's
Width: 30cm's
Thrust Development: 6,420kg's
Nozzle Arrangement: 3D thrust vectoring; 45*
Description: Long Range AAM; Mach 4 to 5, range of 150 to 205 miles.

NP-M-110 Hybrid
Dry Weight: 310kgs
Length: 82cm's
Width: 34cm's
Thrust Development: 9,420kg's
Nozzle Arrangement: 3D thrust vectoring; 45*
Description: Long Range AAM; Speed of Mach 5 to Mach 7 using both Pulse Detonation Engines (PDE) and SCRAMjet in a hybrid fashion. Range estimated at 270 miles.

NP-M-120 Hybrid
Dry Weight: 405kgs
Length: 1.082m's
Width: 0.434m's
Thrust Development: 12,176kg's
Nozzle Arrangement: 3D thrust vectoring; 45*
Description: Long Range ASM or Land Attack; Speed of Mach 5 to Mach 7 using both Pulse Detonation Engines (PDE) and SCRAMjet in a hybrid fashion. Range estimated at 400+ miles.

Bah. These are vastly superior to any Pratt & Whittney engine, and can replace the ones currently installed on F-15's, 16's, 18's and 22's. Same goes for Russians.

tag. This looks like a VERY interesting storefront

bump! I'll be adding Scramjet and RAMjet propulsion for missiles as well as hybrid Pulse-Det engines.

bump!

Added Missile engines!

Statement from the Dept. of Defense

"At this time, the Militant Imperium seeks to acquire hafnium-based engines for our development in long-range reconnaisance vehicles. Our own attempts at adapting hafnium isomers to this task have failed miserably; thus, we wish to purchase five NP-999-QNF powerplants for testing. If our designs are successful, a larger order will inevitably follow.

Money has been wired to Nonlan-Petyav Aerospace's bank account in advance."

To: Tyrandis DoD
From: The desk of Nolan & Petyav
Re: NP-999-QNF

We will sell you five of the NP-999-QNF powerplants, for a total of $8,750,000. Now, we are prepared to send N&P engineers to assist you in the intragration to your aircraft. If however the NP-999-QNF does not fit your needs, we are capable of producing custom engines - at a price.

Bump For Missile Powerplants!!

got a J79 replacement?

I do indeed. The J79 doesn't develop any thrust even close to our cheapest engine.

I would like to buy the production rights for you hafnium assist engines and your SCRAMJET/Hafnium Hybrids.

(ooc: how much does the Hybrid cost?)

the NP-999-QNF is $605,000,000 for prod rights, and the (I assume you meant PDE not Hafnium) Hybrid Missile engine is $400,000,000 for a grand total of:
$1,000,000,000.

Order confirmed.

I do indeed. The J79 doesn't develop any thrust even close to our cheapest engine.
Well i know that, but do you have anything to fit its dimentions?

The Nation of the SovietRepublicofRussia would like to purchase the following:

NP-999-QNF Hafnium Production Rights-$605,000,000
NP-1707-QNF Hafnium Propellant Production Rights-$650,000,000


totaling: 1,255,000,000

Confirmed SRoR.

Seversky, I would say the NP-62 or 63. (62 is single engine and 63 is meant for pairs)

*money wired*

From: ALPHAtech Research & Development; Section 3
To: The desk of Nolan & Petyav

Dear Sirs & Madams,

ALPHATech Industries is currently in process of developing a compact Man-Pac Surface to Air Version of its AIM-103X MADRAAM. This is obviously no easy task, and we require a Light weight Soft-launch capable solid rocket engine capable of providing ranges and alititudes greater than six thousand meters and velocity greater than Mach 3.5. The motor should also be able to continue sustained propulsion during turns in excess of 9 G's.

This rocket motor will be placed at the end of an 8x14 inch diameter gimbled section at the rear of the rocket to provide high manuverability to the missile, and will preferably less than 8kgs in weight. If you beleive you are capable of developing such a motor please let us know so that we can discuss the cost of such a motor on a per unit basis as this is a comercial venture.

If you think you can achieve such preformance within the weight limits please let us know as we would be highly interested in contracting the production of such a motor with final assembly of the system to be accomplished in Mekugi.

Sincerely,
-William Schaffer
ATI R&D

((OOC: full credit will be given and a link will be listed in the write up for the unit.))

N&P Engineers will gladly take this assignment, and we will immediatly begin. How do you feel about Pulse Detonation Engines?

We would prefer a sustained thrust method due to both the space, and weight requirments, But are willing to entertain several entries as long as the requirments are met.

ooc: I won't be able to get around to this until tomarrow. I have a fiendish amount of hmwk.

((OOC: quite alright, I just wanted to put the contract out there so I can move on with other projects.))

NP-M-96E Rocket
Dry Weight: 9kgs
Length: 14"
Width: 6.5"
Thrust Developed: 1,688kg's at Sea Level (Should get you to Mach 4)
Nozzle Arrangement: 3D Thrust Vectored; Vertical: -45*, +45;
Fuel Efficiancy: 1kg of fuel used = 1,250m
Fuel Intended: 10kgs
Description: Uses a solid fuel propellent, and an incredible 3D thrust vectoring system for added maneuverability. The engine itself is made out of incredibly strong metals, the engine can withstand close to 20G's.
Price: $84,000; Production Rights: $8,000,000

TOTAL WEIGHT OF UNIT: 19kg's

((OOC; very nice, infact it may have just overqualified itself... :eek: ))

We thank you for your prompt reply and would like to purchase production rights for this motor for future plans... however... The motor we had originally contacted you about was intended for instalation in a shoulder lauched Surface to Air Missile, and although the stats are above and beyond the initial requirements it would mean the final product would be over 45 pounds with guidance, warhead, and firing tube. Which for a squad based weapon is rather hefty.

In short what we need is actually a less impressive lighter weight system (actually just lighter weight) though we are able to make concessions on range, and structural integrity (20g's is impressive but for a disposable weapon, overkill)

Prefferably around 10 kg's would be the preffered weight, carrying 8 kg's of fuel at its current efficiency to provide a range of 10km to the system. The nozzle itself can be fixed as the rear fuel section of the missile aeroframe that the motor will be installed into is gimbled allowing for similar results (though a combined 90* 3d thrust vectoring would be scary as hell ^_^)We also realized that in our haste we have misqouted the size restraints it should be no larger than 3.5x14 inches. Though we are quite pleased with the results, and await a possible solution, and look forward to future buisness.

Sincerely,
-William Schaffer
ATI R&D

-An account transaction of 8000000.00 USD has been sent-

We can easily change the materials in which we used, but it will lower the G rating to around 10. That should give you the desired weight.

We can easily change the materials in which we used, but it will lower the G rating to around 10. That should give you the desired weight.

That would be excellant. A lowered cost per unit production as well we hope, that still can meet the requirments is exactly what were looking for; considering it is to be a one shot per tube weapon.

(( I also realized I mis-stated the size and appologize greatly, it should be no larger than 4x14inches. I really need to stop mixing up requirments as im also working on a ATGW write up that was 8 inches, as an 8 inch diameter Shoulder launched missile would be quite a bruiser.))

Bump!

Bump!!

Bump

From: Castor Draaga,
Imperial Minister of Security,
The Holy Empire of Streleheim

To: Nolan-Petyav Aerospace Propulsion Industries

Subject: Streleheim Purchases

The Holy Empire of Streleheim wishes to purchase ten (10) NP-21E Turbojets. This would amount to the total sum of $ 6500,000.

Confirmed

1100 NP-62s and a shoe horn please.

*wired.*

You are confirmed.

Statement from the Dept. of Defense

TO: Nolan-Petyav Aerospace Propulsion Industries:

We were successful in using the NP-999 Hafnium engine with our RVQA-25 Bandit Antiradar UCAV. Initial trials of the new machine showed that using the Artitsan engine improved the vehicle's range by an order of magnitude.

Thus, we formally request to purchase production rights, and will wire the money to your bank account as soon as the we receive the plans.

We are always pleased to business with our friends in Tyrandis, your order is confirmed.

We are always pleased to business with our friends in Tyrandis, your order is confirmed.

The $605 million USD has been wired to your bank account.

Bump

Bump.

bump

Bah. These are vastly superior to any Pratt & Whittney engine, and can replace the ones currently installed on F-15's, 16's, 18's and 22's. Same goes for Russians.

Of course they are. Like if anyone doesn't bump up specs of his engines above all RL ones. It takes just a few key hits, after all. What is never mentioned is why, bah, just increase the numbers.

Don't take seriously, just rant.

Of course they are. Like if anyone doesn't bump up specs of his engines above all RL ones. It takes just a few key hits, after all. What is never mentioned is why, bah, just increase the numbers.

Don't take seriously, just rant.

*pats on head* there there... there there.

*throws into burning pit of death.*