https://www.defensenews.com/industry/te ... ons-plans/In a Japanese-language document published on the Acquisition, Technology and Logistics Agency website, the government said two classes of standoff hypersonic systems will be deployed — the Hypersonic Cruise Missile (HCM) and the Hyper Velocity Gliding Projectile (HVGP).
The former will be powered by a scramjet engine and appears similar to a typical missile, albeit one that cruises at a much higher speed while capable of traveling at long ranges.
The HVGP, on the other hand, will feature a solid-fuel rocket engine that will boost its warhead payload to a high altitude before separation, where it will then glide to its target using its altitude to maintain high velocity until impact.
The agency also provided more details regarding warhead payloads, with different warheads planned for both seaborne and land targets. The former will be an armor-piercing warhead designed specifically for penetrating “the deck of the [aircraft] carrier,” while a land-attack version will utilize a high-density, explosively formed projectile, or EFP, for area suppression.
Area suppression effects for the latter will be achieved via the use of multiple EFPs, which are more commonly known as a shaped charge. An EFP is made up of a concave metal hemispherical or cone-shaped liner backed by a high explosive, all in a steel or aluminum casing. When the high explosive is detonated, the metal liner is compressed and squeezed forward, forming a jet whose tip may travel as fast as 6 miles per second.
Japan’s road map also revealed the country is taking an incremental approach with regard to designing the shapes of warheads and developing solid-fuel engine technology, with plans to field early versions of both in the 2024 to 2028 time frame. They are expected to enter service in the early 2030s.
The agency expects both systems to navigate via satellite navigation with an inertial navigation system as backup. Japan is seeking to establish a network of seven satellites to enable continuous positioning for its self-defense forces, which will enable it to provide continuous navigation data without relying on foreign satellites.
Warhead guidance is achieved via either radio-frequency imaging converted from doppler shift data — which the government agency said will be able to identify stealthy naval targets in all weather conditions — or an infrared seeker capable to discriminating specific targets.
研究開発ビジョン~多次元統合防衛力の実現とその先へ~(令和元年8月)
https://www.mod.go.jp/atla/soubiseisaku_vision.html
- 研究開発ビジョン~多次元統合防衛力の実現とその先へ~解説資料
- スタンド・オフ防衛能力の取組
https://www.mod.go.jp/atla/soubiseisaku ... etsu05.pdf
- スタンド・オフ防衛能力の取組
島嶼防衛用高速滑空弾の研究
https://www.mod.go.jp/atla/soubi_system.html
「スクラムジェットエンジンの研究
https://www.mod.go.jp/atla/kousouken.html
ヅ工ツト雑料 … Illustration of construction
燃料タノク … Fuel tank
弾頭 … Warhead
Scramjet engne research「スクラムジェットエンジンの研究」
将来の誘導弾への適用を目指し、従来のエンジン技術では実現できなかった高高度極超音速(マッハ5以上)巡航を可能とする「スクラムジェットエンジンの研究」を実施しています。
本研究では、装備品としての実現に留意し、従来までの研究の主流であった水素燃料に比べ、機体規模の小型化、入手性・貯蔵・取扱の容易さに大幅に優れる炭化水素燃料(ジェット燃料)を採用するとともに、超音速から極超音速までの幅広い速度域での作動を実現する、ラムモードとスクラムモードの2つのモードによるデュアルモード・スクラムジェットエンジンの実現を目指しています。
炭化水素燃料を用いたスクラムジェットエンジンの成立性の検証のため、JAXAとの研究協力の下、燃焼試験を行い、ジェット燃料によるスクラム燃焼に成功するとともに、冷却系検討に資する基礎データを取得しました。
これらの研究成果に基づき、実飛しょうを想定したスクラムジェットエンジンシステムの研究に取り組んでいます。
With the aim of applying it to future guided missiles, we are conducting “Scramjet engine research” that enables high altitude hypersonic (Mach 5 or more) cruising that was not possible with conventional engine technology.
In this research, attention was paid to the realization as equipment, and compared to hydrogen fuel, which has been the mainstream of previous research, hydrocarbon fuel (which is significantly superior in miniaturization of the fuselage scale and ease of availability, storage, and handling ( We are aiming to realize a dual-mode scramjet engine with two modes, a ram mode and a scram mode, that operate in a wide speed range from supersonic to hypersonic speeds while adopting jet fuel.
Based on these research results, we are working on research on a scramjet engine system assuming actual flight.